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All Classes All Packages

A

a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final semi major axis.

a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

a.

A - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

A = sqrt(μ * a).

a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original recovered semi major axis.

AbsoluteDate - Class in org.orekit.time

This class represents a specific instant in time.

AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate

Create an instance with a default value (AbsoluteDate.J2000_EPOCH).

AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location (parsed from a string) in a time scale.

AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from an elapsed duration since to another instant.

AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.

AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive

Parameter name for absorption coefficient.

AbstractAnalyticalPropagator - Class in org.orekit.propagation.analytical

Common handling of Propagator methods for analytical propagators.

AbstractAnalyticalPropagator(AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Build a new instance.

AbstractCovarianceMatrixProvider - Class in org.orekit.estimation.sequential

Abstract provider handling a predefined initial covariance matrix.

AbstractCovarianceMatrixProvider(RealMatrix) - Constructor for class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider

Simple constructor.

AbstractDetector<T extends EventDetector> - Class in org.orekit.propagation.events

Common parts shared by several orbital events finders.

AbstractDetector(double, double, int, EventHandler<? super T>) - Constructor for class org.orekit.propagation.events.AbstractDetector

Build a new instance.

AbstractForceModel - Class in org.orekit.forces

Base class for force models.

AbstractForceModel() - Constructor for class org.orekit.forces.AbstractForceModel

AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces

Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.

AbstractGaussianContribution(String, double, ForceModel) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Build a new instance.

AbstractGNSSAttitudeProvider - Class in org.orekit.gnss.attitude

Base class for attitude providers for navigation satellites.

AbstractGNSSAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider

Simple constructor.

AbstractIntegratedPropagator - Class in org.orekit.propagation.integration

Common handling of Propagator methods for both numerical and semi-analytical propagators.

AbstractIntegratedPropagator(ODEIntegrator, boolean) - Constructor for class org.orekit.propagation.integration.AbstractIntegratedPropagator

Build a new instance.

AbstractIntegratedPropagator.MainStateEquations - Interface in org.orekit.propagation.integration

Differential equations for the main state (orbit, attitude and mass).

AbstractMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements

Abstract class handling measurements boilerplate.

AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<Integer>, ParameterDriver...) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement

Deprecated.

since 9.3, replaced bew AbstractMeasurement(AbsoluteDate, double[], double[], double[], List) followed by AbstractMeasurement.addParameterDriver(ParameterDriver)

AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement

Simple constructor, for multi-dimensional measurements.

AbstractMeasurement(AbsoluteDate, double, double, double, List<Integer>, ParameterDriver...) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement

Deprecated.

since 9.3, replaced bew AbstractMeasurement(AbsoluteDate, double, double, double, List) followed by AbstractMeasurement.addParameterDriver(ParameterDriver)

AbstractMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement

Simple constructor for mono-dimensional measurements.

AbstractMeasurementBuilder<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation

Base class for measurements builders.

AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double[], double[], ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Simple constructor.

AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Simple constructor.

AbstractParametricAcceleration - Class in org.orekit.forces

This class implements a parametric acceleration.

AbstractParametricAcceleration(Vector3D, boolean, AttitudeProvider) - Constructor for class org.orekit.forces.AbstractParametricAcceleration

Simple constructor.

AbstractPropagator - Class in org.orekit.propagation

Common handling of Propagator methods for analytical propagators.

AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator

Build a new instance.

AbstractPropagatorBuilder - Class in org.orekit.propagation.conversion

Base class for propagator builders.

AbstractPropagatorBuilder(Orbit, PositionAngle, double, boolean) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Build a new instance.

AbstractPropagatorConverter - Class in org.orekit.propagation.conversion

Common handling of PropagatorConverter methods for propagators conversions.

AbstractPropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorConverter

Build a new instance.

AbstractScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation

Base implementation of Scheduler managing dates selection.

AbstractScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.AbstractScheduler

Simple constructor.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.AbstractParametricAcceleration

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.AbstractParametricAcceleration

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Compute acceleration.

acceptStep(FieldAbstractAnalyticalPropagator.FieldBasicStepInterpolator, FieldAbsoluteDate<T>, double) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Accept a step, triggering events and step handlers.

acceptStep(OrekitStepInterpolator, AbsoluteDate, double) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Accept a step, triggering events and step handlers.

AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for AdamsBashforthIntegrator.

AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder

Build a new instance.

AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for AdamsMoultonIntegrator.

AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder

Build a new instance.

AdapterDetector - Class in org.orekit.propagation.events

Base class for adapting an existing detector.

AdapterDetector(EventDetector) - Constructor for class org.orekit.propagation.events.AdapterDetector

Build an adaptor wrapping an existing detector.

AdapterPropagator - Class in org.orekit.propagation.analytical

Orbit propagator that adapts an underlying propagator, adding differential effects.

AdapterPropagator(Propagator) - Constructor for class org.orekit.propagation.analytical.AdapterPropagator

Build a propagator from an underlying reference propagator.

AdapterPropagator.DifferentialEffect - Interface in org.orekit.propagation.analytical

Interface for orbit differential effects.

add(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer

Add a step handler.

add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer

Add a step handler.

add(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Add the argument matrix with the current matrix.

add(ParameterDriver) - Method in class org.orekit.utils.ParameterDriversList

Add a driver.

addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Add a set of user-specified equations to be integrated along with the orbit propagation.

addAdditionalEquations(FieldAdditionalEquations<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Add a set of user-specified equations to be integrated along with the orbit propagation.

addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState

Add an additional state.

addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState

Add an additional state.

addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in interface org.orekit.propagation.FieldPropagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add a loader for celestial bodies.

addChild(OrphanFrame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame

Add a child.

addChild(OrphanFrame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame

Add a child.

addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Add the contribution of the wave to Stokes coefficients.

addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in interface org.orekit.forces.ForceModel

Compute the contribution of the force model to the perturbing acceleration.

addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute the contribution of the force model to the perturbing acceleration.

addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Compute the contribution of the force model to the perturbing acceleration.

addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add the default loaders for all predefined celestial bodies.

addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add the default loaders for celestial bodies.

addDefaultEOP1980HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory

Add the default loaders EOP history (IAU 1980 precession/nutation).

addDefaultEOP2000HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory

Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).

addDefaultOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add the default READERS for ocean tides.

addDefaultPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add the default readers for gravity fields.

addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager

Add the default providers configuration.

addDefaultUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory

Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).

addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Add a differential effect.

addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Static method in class org.orekit.frames.FramesFactory

Add a loader for Earth Orientation Parameters history.

addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector

Add an event date.

addEventDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldDateDetector

Add an event date.

addEventDetector(D) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Add an event detector.

addEventDetector(D) - Method in class org.orekit.propagation.FieldAbstractPropagator

Add an event detector.

addEventDetector(D) - Method in interface org.orekit.propagation.FieldPropagator

Add an event detector.

addEventDetector(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Add an event detector.

addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Add an event detector.

addEventDetector(T) - Method in class org.orekit.propagation.AbstractPropagator

Add an event detector.

addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Add an event detector.

addEventDetector(T) - Method in interface org.orekit.propagation.Propagator

Add an event detector.

addFilter(DataFilter) - Method in class org.orekit.data.DataProvidersManager

Add a data filter.

addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Add a force model to the global perturbation model.

addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Add a force model to the global perturbation model.

addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Add a force model.

addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Add a force model to the global perturbation model.

addGridPoint(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Add a point to the interpolation grid.

ADDITIONAL_STATE_NAME_ALREADY_IN_USE - org.orekit.errors.OrekitMessages

AdditionalEquations - Interface in org.orekit.propagation.integration

This interface allows users to add their own differential equations to a numerical propagator.

AdditionalStateProvider - Interface in org.orekit.propagation

This interface represents providers for additional state data beyond SpacecraftState.

addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations

Add the contribution of the Kepler evolution.

addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of the Kepler evolution.

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CircularOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.Orbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of the flow rate (dm/dt).

addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations

Add the contribution of the flow rate (dm/dt).

addMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Add a measurement.

addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Add a modifier.

addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Add a modifier.

addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Add a modifier.

addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Add a modifier.

addNewSegment(List<SpacecraftState>) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

addNewSegment(List<SpacecraftState>, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

addNewSegment(List<SpacecraftState>, CelestialBody, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

addNonKeplerianAcceleration(FieldVector3D<T>) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations

Add the contribution of an acceleration expressed in some inertial frame.

addNonKeplerianAcceleration(Vector3D) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of a non-Keplerian acceleration.

addObservation(String, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Adds an observation data line.

addObservation(TDMFile.Observation) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Adds an observation data line.

addObservationComment(String) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Add an observation data line comment.

addObservationsBlock() - Method in class org.orekit.files.ccsds.TDMFile

Add a block to the list of observations blocks.

addObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver

Add an observer for this driver.

addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add a reader for ocean tides.

addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Add an offset from the instance.

addOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Add an offset from the instance.

addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Add an offset from the instance.

addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Add an offset from the instance.

addParameterDriver(ParameterDriver) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Add a parameter driver.

addParticipant(int, String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Adds a participant to the list.

addPoint(AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic

Add a fitting point.

addPotentialCoefficientsReader(PotentialCoefficientsReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add a reader for gravity fields.

addPropagationConfiguration(NumericalPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Add a propagation configuration.

addPropagator(Propagator) - Method in class org.orekit.estimation.measurements.generation.Generator

Add a propagator.

addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Add a data provider to the supported list.

addReceiveDelay(int, double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Adds a receive delay to the list.

addSatellite(String) - Method in class org.orekit.files.general.OrekitEphemerisFile

Adds a new satellite to this object.

addSatellite(String) - Method in class org.orekit.files.sp3.SP3File

Add a new satellite with a given identifier to the list of stored satellites.

addScheduler(Scheduler<T>) - Method in class org.orekit.estimation.measurements.generation.Generator

Add a sequences generator for a specific measurement type.

addSupportedParameter(ParameterDriver) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Add a supported parameter.

addSwitchingCondition(AttitudeProvider, AttitudeProvider, T, boolean, boolean, double, AngularDerivativesFilter, AttitudesSequence.SwitchHandler) - Method in class org.orekit.attitudes.AttitudesSequence

Add a switching condition between two attitude providers.

addTransmitDelay(int, double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Adds a transmit delay to the list.

addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Static method in class org.orekit.time.TimeScalesFactory

Add a loader for UTC-TAI offsets history files.

addValidAfter(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Add an entry valid after a limit date.

addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap

Add an entry valid after a limit date.

addValidBefore(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Add an entry valid before a limit date.

addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap

Add an entry valid before a limit date.

addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Add parsed coefficients.

afterIntegration() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Method called just after integration.

afterIntegration() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Method called just after integration.

afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Method called just after integration.

AggregateBoundedPropagator - Class in org.orekit.propagation.analytical

A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.

AggregateBoundedPropagator(Collection<? extends BoundedPropagator>) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator

Create a propagator by concatenating several BoundedPropagators.

AlignmentDetector - Class in org.orekit.propagation.events

Finder for satellite/body alignment events in orbital plane.

AlignmentDetector(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Build a new alignment detector.

AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Build a new alignment detector.

AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Build a new alignment detector.

ALMOST_CRITICALLY_INCLINED_ORBIT - org.orekit.errors.OrekitMessages

ALMOST_EQUATORIAL_ORBIT - org.orekit.errors.OrekitMessages

alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming

Find the along tile direction for tessellation at specified point.

alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming

Find the along tile direction for tessellation at specified point.

alongTileDirection(Vector3D, GeodeticPoint) - Method in interface org.orekit.models.earth.tessellation.TileAiming

Find the along tile direction for tessellation at specified point.

AlongTrackAiming - Class in org.orekit.models.earth.tessellation

Class used to orient tiles along an orbit track.

AlongTrackAiming(OneAxisEllipsoid, Orbit, boolean) - Constructor for class org.orekit.models.earth.tessellation.AlongTrackAiming

Simple constructor.

ALTITUDE_BELOW_ALLOWED_THRESHOLD - org.orekit.errors.OrekitMessages

AltitudeDetector - Class in org.orekit.propagation.events

Finder for satellite altitude crossing events.

AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

andCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that is the logical AND of the given event detectors.

andCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that is the logical AND of the given event detectors.

ANGLE_1 - org.orekit.files.ccsds.Keyword

Data: ANGLE_1 in degrees and in [-180, +360[ [deg].

ANGLE_2 - org.orekit.files.ccsds.Keyword

Data: ANGLE_2 in degrees and in [-180, +360[ [deg].

ANGLE_TYPE - org.orekit.files.ccsds.Keyword

Meta-data: The ANGLE_TYPE keyword shall indicate the type of antenna geometry represented in the angle data (ANGLE_1 and ANGLE_2 keywords).

ANGLE_TYPE_NOT_SUPPORTED - org.orekit.errors.OrekitMessages

AngularAzEl - Class in org.orekit.estimation.measurements

Class modeling an Azimuth-Elevation measurement from a ground station.

AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.AngularAzEl

Deprecated.

since 9.3, replaced by AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], ObservableSatellite)

AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], int) - Constructor for class org.orekit.estimation.measurements.AngularAzEl

Deprecated.

since 9.3, replaced by AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], ObservableSatellite)

AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularAzEl

Simple constructor.

AngularAzElBuilder - Class in org.orekit.estimation.measurements.generation

Builder for AngularAzEl measurements.

AngularAzElBuilder(CorrelatedRandomVectorGenerator, GroundStation, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularAzElBuilder

Simple constructor.

AngularCoordinates - Class in org.orekit.utils

Simple container for rotation/rotation rate/rotation acceleration triplets.

AngularCoordinates() - Constructor for class org.orekit.utils.AngularCoordinates

Simple constructor.

AngularCoordinates(FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a AngularCoordinates from a FieldRotation<DerivativeStructure>.

AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a rotation/rotation rate pair.

AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a rotation/rotation rate/rotation acceleration triplet.

AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates

Build one of the rotations that transform one pv coordinates into another one.

AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another one.

AngularDerivativesFilter - Enum in org.orekit.utils

Enumerate for selecting which derivatives to use in TimeStampedAngularCoordinates and TimeStampedFieldAngularCoordinates interpolation.

AngularIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical angular measurement with ionospheric delay.

AngularIonosphericDelayModifier(IonosphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier

Constructor.

AngularRaDec - Class in org.orekit.estimation.measurements

Class modeling an Right Ascension - Declination measurement from a ground point (station, telescope).

AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.AngularRaDec

Deprecated.

since 9.3, replaced by AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite)

AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], int) - Constructor for class org.orekit.estimation.measurements.AngularRaDec

Deprecated.

since 9.3, replaced by AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite)

AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularRaDec

Simple constructor.

AngularRaDecBuilder - Class in org.orekit.estimation.measurements.generation

Builder for AngularRaDec measurements.

AngularRaDecBuilder(CorrelatedRandomVectorGenerator, GroundStation, Frame, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularRaDecBuilder

Simple constructor.

AngularRadioRefractionModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical angular measurement with ionospheric radio refractive index.

AngularRadioRefractionModifier(AtmosphericRefractionModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier

Constructor.

AngularSeparationDetector - Class in org.orekit.propagation.events

Detects when spacecraft comes close to a moving beacon, as seen from a moving observer.

AngularSeparationDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector

Build a new angular separation detector.

AngularTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical angular measurement with tropospheric delay.

AngularTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier

Constructor.

Antenna - Class in org.orekit.gnss.antenna

GNSS antenna model.

Antenna(String, String, Map<Frequency, FrequencyPattern>) - Constructor for class org.orekit.gnss.antenna.Antenna

Simple constructor.

AntexLoader - Class in org.orekit.gnss.antenna

Factory for GNSS antennas (both receiver and satellite).

AntexLoader(String) - Constructor for class org.orekit.gnss.antenna.AntexLoader

Simple constructor.

apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the effect of the maneuver on an orbit.

apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect

Compute the effect of the maneuver on an orbit.

apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the effect of the maneuver on a spacecraft state.

apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect

Apply the effect to a spacecraft state.

apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect

Apply the effect to a spacecraft state.

apply(SpacecraftState) - Method in interface org.orekit.propagation.events.FunctionalDetector.GFunction

Deprecated.

Use ToDoubleFunction.applyAsDouble(Object) instead. Will be removed in next major release.

applyAllFilters(NamedData) - Method in class org.orekit.data.DataProvidersManager

Apply all the relevant data filters, taking care of layers.

applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(PVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates

Apply the rotation to a pv coordinates.

approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic

Approximate an already fitted model to polynomial only terms.

APRIL - org.orekit.time.Month

April.

ApsideDetector - Class in org.orekit.propagation.events

Finder for apside crossing events.

ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector

Build a new instance.

ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector

Build a new instance.

ARC_SECONDS - org.orekit.data.PolynomialParser.Unit

Arc-seconds angles.

ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants

Conversion factor from arc seconds to radians: 2*PI/(360*60*60).

ARG_OF_PERICENTER - org.orekit.files.ccsds.Keyword

Orbit argument of pericenter.

ASTRONOMICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector

Sun elevation at astronomical dawn/dusk (18° below horizon).

AstronomicalAmplitudeReader - Class in org.orekit.forces.gravity.potential

Parser for tides astronomical amplitude H_f.

AstronomicalAmplitudeReader(String, int, int, int, double) - Constructor for class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Simple constructor.

Atmosphere - Interface in org.orekit.forces.drag.atmosphere

Interface for atmospheric models.

AtmosphericRefractionModel - Interface in org.orekit.models

Defines an refraction model that can be used to correct for the apparent position of an object due to atmospheric effects.

ATOMIC_NITROGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000

Identifier for atomic nitrogen.

ATOMIC_OXYGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000

Identifier for atomic oxygen.

attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame

Attach the instance (and all its children down to leafs) to the main tree.

attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame

Attach the instance (and all its children down to leafs) to the main tree.

Attitude - Class in org.orekit.attitudes

This class handles attitude definition at a given date.

Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND - org.orekit.errors.OrekitMessages

attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder

Sets the attitude provider.

AttitudeProvider - Interface in org.orekit.attitudes

This interface represents an attitude provider model set.

AttitudeProviderModifier - Interface in org.orekit.attitudes

This interface represents an attitude provider that modifies/wraps another underlying provider.

AttitudesSequence - Class in org.orekit.attitudes

This classes manages a sequence of different attitude providers that are activated in turn according to switching events.

AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence

Constructor for an initially empty sequence.

AttitudesSequence.SwitchHandler - Interface in org.orekit.attitudes

Interface for attitude switch notifications.

ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction

Suffix for parameter name for attraction coefficient enabling Jacobian processing.

AUGUST - org.orekit.time.Month

August.

AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities

Container class for common parameters used by all DSST forces.

AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Simple constructor.

AVERAGE - org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel

Average level of activity.

B

B - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

B = sqrt(1 - h² - k²).

B_STAR - Static variable in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Parameter name for B* coefficient.

B01 - org.orekit.gnss.Frequency

Beidou B1 (1561.098 MHz).

B02 - org.orekit.gnss.Frequency

Beidou B2 (1207.14 MHz).

B03 - org.orekit.gnss.Frequency

Beidou B3 (1268.52 MHz).

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Propagate an orbit without any fancy features.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Propagate an orbit without any fancy features.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Propagate an orbit without any fancy features.

basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Propagate an orbit without any fancy features.

basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Propagate an orbit without any fancy features.

BatchLSEstimator - Class in org.orekit.estimation.leastsquares

Least squares estimator for orbit determination.

BatchLSEstimator(LeastSquaresOptimizer, NumericalPropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.BatchLSEstimator

Simple constructor.

BatchLSObserver - Interface in org.orekit.estimation.leastsquares

Observer for batch least squares estimator iterations.

BCT - org.orekit.files.sp3.SP3File.SP3OrbitType

broadcast.

BDTScale - Class in org.orekit.time

Beidou system time scale.

beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Method called just before integration.

beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Method called just before integration.

beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Method called just before integration.

BEIDOU - org.orekit.gnss.SatelliteSystem

Beidou system.

BEIDOU_2G - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

BeiDou-2 GEO.

BEIDOU_2G - org.orekit.gnss.antenna.SatelliteType

BeiDou-2 GEO.

BEIDOU_2I - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

BeiDou-2 IGSO.

BEIDOU_2I - org.orekit.gnss.antenna.SatelliteType

BeiDou-2 IGSO.

BEIDOU_2M - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

BeiDou-2 MEO.

BEIDOU_2M - org.orekit.gnss.antenna.SatelliteType

BeiDou-2 MEO.

BEIDOU_3I - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

BeiDou-3 IGSO.

BEIDOU_3I - org.orekit.gnss.antenna.SatelliteType

BeiDou-3 IGSO.

BeidouGeo - Class in org.orekit.gnss.attitude

Attitude providers for Beidou geostationary orbit navigation satellites.

BeidouGeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouGeo

Simple constructor.

BeidouIGSO - Class in org.orekit.gnss.attitude

Attitude providers for Beidou inclined geosynchronous orbit navigation satellites.

BeidouIGSO(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouIGSO

Simple constructor.

BeidouMeo - Class in org.orekit.gnss.attitude

Attitude providers for Beidou Medium Earth Orbit navigation satellites.

BeidouMeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouMeo

Simple constructor.

BESSELIAN_YEAR - Static variable in interface org.orekit.utils.Constants

Duration of a Besselian year: 365.242198781 Constants.JULIAN_DAY.

beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

sqrt (1 - e2).

beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

1 - e2.

Bias<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers

Class modeling a measurement bias.

Bias(String[], double[], double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.modifiers.Bias

Simple constructor.

BLOCK_I - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GPS Block I : SVN 01-11.

BLOCK_I - org.orekit.gnss.antenna.SatelliteType

GPS Block I : SVN 01-11.

BLOCK_II - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GPS Block II : SVN 13-21.

BLOCK_II - org.orekit.gnss.antenna.SatelliteType

GPS Block II : SVN 13-21.

BLOCK_IIA - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GPS Block IIA : SVN 22-40.

BLOCK_IIA - org.orekit.gnss.antenna.SatelliteType

GPS Block IIA : SVN 22-40.

BLOCK_IIF - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GPS Block IIF : SVN 62-73.

BLOCK_IIF - org.orekit.gnss.antenna.SatelliteType

GPS Block IIF : SVN 62-73.

BLOCK_IIIA - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GPS Block IIIA : SVN 74-81.

BLOCK_IIIA - org.orekit.gnss.antenna.SatelliteType

GPS Block IIIA : SVN 74-81.

BLOCK_IIR_A - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GPS Block IIR : SVN 41, 43-46, 51, 54, 56.

BLOCK_IIR_A - org.orekit.gnss.antenna.SatelliteType

GPS Block IIR : SVN 41, 43-46, 51, 54, 56.

BLOCK_IIR_B - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GPS Block IIR : SVN 47, 59-61.

BLOCK_IIR_B - org.orekit.gnss.antenna.SatelliteType

GPS Block IIR : SVN 47, 59-61.

BLOCK_IIR_M - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GPS Block IIR-M : SVN 48-50, 52-53, 55, 57-58.

BLOCK_IIR_M - org.orekit.gnss.antenna.SatelliteType

GPS Block IIR-M : SVN 48-50, 52-53, 55, 57-58.

BodiesElements - Class in org.orekit.data

Elements of the bodies having an effect on nutation.

BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements

Simple constructor.

body - org.orekit.files.ccsds.Keyword

Body keyword.

BodyCenterPointing - Class in org.orekit.attitudes

This class handles body center pointing attitude provider.

BodyCenterPointing(Frame, Ellipsoid) - Constructor for class org.orekit.attitudes.BodyCenterPointing

Creates new instance.

BodyShape - Interface in org.orekit.bodies

Interface representing the rigid surface shape of a natural body.

BooleanDetector - Class in org.orekit.propagation.events

This class provides AND and OR operations for event detectors.

BoundedPropagator - Interface in org.orekit.propagation

This interface is intended for ephemerides valid only during a time range.

BoxAndSolarArraySpacecraft - Class in org.orekit.forces

Class representing the features of a classical satellite with a convex body shape and rotating flat solar arrays.

BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with best lighting of solar array.

BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with best lighting of solar array.

BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with linear rotation of solar array.

BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with linear rotation of solar array.

BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with best lighting of solar array.

BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with best lighting of solar array.

BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with linear rotation of solar array.

BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with linear rotation of solar array.

BoxAndSolarArraySpacecraft.Facet - Class in org.orekit.forces

Class representing a single facet of a convex spacecraft body.

BSTAR - org.orekit.files.ccsds.Keyword

SGP/SGP4 drag-like coefficient.

build() - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Construct a KalmanEstimator from the data in this builder.

build() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder

Finalizes the build.

build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.AngularAzElBuilder

Generate a single measurement.

build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.AngularRaDecBuilder

Generate a single measurement.

build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder

Generate a single measurement.

build(SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Generate a single measurement.

build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.PositionBuilder

Generate a single measurement.

build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.PVBuilder

Generate a single measurement.

build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.RangeBuilder

Generate a single measurement.

build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.RangeRateBuilder

Generate a single measurement.

build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder

Generate a single measurement.

buildAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Method in enum org.orekit.gnss.antenna.SatelliteType

Build an attitude provider suitable for this satellite type.

Builder(GPSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder

Initializes the builder.

buildIdentityMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the identity matrix of order 2.

buildIdentityMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the identity matrix of order 4.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder

Build a first order integrator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Build a propagator.

buildRow(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Build a coefficients row.

buildSimpleZone(double, double[]...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Build a simple zone (connected zone without holes).

buildSimpleZone(double, GeodeticPoint...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Build a simple zone (connected zone without holes).

buildTriangularArray(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Build a coefficients triangular array.

buildZeroMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the empty matrix of order 2.

buildZeroMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the empty matrix of order 4.

BULLETINA_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinA files (IAU1980 and IAU2000 compatibles).

BULLETINB_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinB files (IAU1980 compatibles).

BULLETINB_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinB files (IAU2000 compatibles).

BurstSelector - Class in org.orekit.time

Selector generating high rate bursts of dates separated by some rest period.

BurstSelector(int, double, double, TimeScale) - Constructor for class org.orekit.time.BurstSelector

Simple constructor.

C

C - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

C = 1 + p² + q².

C01 - org.orekit.gnss.Frequency

In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).

C02 - org.orekit.gnss.Frequency

In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).

C06 - org.orekit.gnss.Frequency

In the ANTEX files, C06 appears without much reference, we assume it is B2 (1207.14 MHz).

C07 - org.orekit.gnss.Frequency

In the ANTEX files, C07 seems to refer to a signal close to E06, probably B3...

c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C1 from SPTRCK #3.

C1 - org.orekit.gnss.ObservationType

Pseudorange GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.

C1A - org.orekit.gnss.ObservationType

Pseudorange Galileo E1 A for Rinex3.

C1B - org.orekit.gnss.ObservationType

Pseudorange Galileo E1 I/NAV OS/CS/SoL for Rinex3.

C1C - org.orekit.gnss.ObservationType

Pseudorange GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.

C1I - org.orekit.gnss.ObservationType

Pseudorange Beidou B1 I for Rinex3.02.

C1L - org.orekit.gnss.ObservationType

Pseudorange GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3.

C1M - org.orekit.gnss.ObservationType

Pseudorange GPS L1 M for Rinex3.

C1P - org.orekit.gnss.ObservationType

Pseudorange GPS L1 P(AS off) / GLONASS G1 P for Rinex3.

C1Q - org.orekit.gnss.ObservationType

Pseudorange Beidou B1 Q for Rinex3.02.

C1S - org.orekit.gnss.ObservationType

Pseudorange GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3.

C1W - org.orekit.gnss.ObservationType

Pseudorange GPS L1 Z-tracking and similar (AS on) for Rinex3.

C1X - org.orekit.gnss.ObservationType

Pseudorange GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) for Rinex3.

C1Y - org.orekit.gnss.ObservationType

Pseudorange GPS L1 Y for Rinex3.

C1Z - org.orekit.gnss.ObservationType

Pseudorange Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3.

c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C2 from SPTRCK #3.

C2 - org.orekit.gnss.ObservationType

Pseudorange GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.

C2C - org.orekit.gnss.ObservationType

Pseudorange GPS L2 C/A / GLONASS G2 C/A for Rinex3.

C2D - org.orekit.gnss.ObservationType

Pseudorange GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.

C2I - org.orekit.gnss.ObservationType

Pseudorange Beidou B1 I for Rinex3.03.

C2L - org.orekit.gnss.ObservationType

Pseudorange GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.

C2M - org.orekit.gnss.ObservationType

Pseudorange GPS L2 M for Rinex3.

C2P - org.orekit.gnss.ObservationType

Pseudorange GPS L2 P(AS off) / GLONASS G2 P for Rinex3.

C2Q - org.orekit.gnss.ObservationType

Pseudorange Beidou B1 Q for Rinex3.03.

C2S - org.orekit.gnss.ObservationType

Pseudorange GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.

C2W - org.orekit.gnss.ObservationType

Pseudorange GPS L2 Z-tracking and similar (AS on) for Rinex3.

C2X - org.orekit.gnss.ObservationType

Pseudorange GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3.

C2Y - org.orekit.gnss.ObservationType

Pseudorange GPS L2 Y for Rinex3.

C3I - org.orekit.gnss.ObservationType

Pseudorange GLONASS G3 I for Rinex3.

C3Q - org.orekit.gnss.ObservationType

Pseudorange GLONASS G3 Q for Rinex3.

C3X - org.orekit.gnss.ObservationType

Pseudorange GLONASS G3 I+Q for Rinex3.

c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C4 from SPTRCK #3.

C5 - org.orekit.gnss.ObservationType

Pseudorange GPS L5 / Galileo E5a / SBAS L5 for Rinex2.

C5A - org.orekit.gnss.ObservationType

Pseudorange IRNSS L5 A for Rinex3.

C5B - org.orekit.gnss.ObservationType

Pseudorange IRNSS L5 B for Rinex3.

C5C - org.orekit.gnss.ObservationType

Pseudorange IRNSS L5 C for Rinex3.

C5I - org.orekit.gnss.ObservationType

Pseudorange GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.

C5Q - org.orekit.gnss.ObservationType

Pseudorange GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.

C5X - org.orekit.gnss.ObservationType

Pseudorange GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C for Rinex3.

C6 - org.orekit.gnss.ObservationType

Pseudorange Galileo E6 / Beidou B03 for Rinex2.

C6A - org.orekit.gnss.ObservationType

Pseudorange Galileo E6 A PRS for Rinex3.

C6B - org.orekit.gnss.ObservationType

Pseudorange Galileo E6 B C/NAV CS for Rinex3.

C6C - org.orekit.gnss.ObservationType

Pseudorange Galileo E6 C no data for Rinex3.

C6I - org.orekit.gnss.ObservationType

Pseudorange Beidou B3 I for Rinex3.

C6L - org.orekit.gnss.ObservationType

Pseudorange QZSS LEX(6) L for Rinex3.

C6Q - org.orekit.gnss.ObservationType

Pseudorange Beidou B3 Q for Rinex3.

C6S - org.orekit.gnss.ObservationType

Pseudorange QZSS LEX(6) S for Rinex3.

C6X - org.orekit.gnss.ObservationType

Pseudorange Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q for Rinex3.

C6Z - org.orekit.gnss.ObservationType

Pseudorange Galileo E6 A+B+C for Rinex3.

C7 - org.orekit.gnss.ObservationType

Pseudorange Galileo E5b / Beidou B02 for Rinex2.

C7I - org.orekit.gnss.ObservationType

Pseudorange Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.

C7Q - org.orekit.gnss.ObservationType

Pseudorange Galileo Q no data / Beidou B2 Q for Rinex3.

C7X - org.orekit.gnss.ObservationType

Pseudorange Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.

C8 - org.orekit.gnss.ObservationType

Pseudorange Galileo E5a+b for Rinex2.

C8I - org.orekit.gnss.ObservationType

Pseudorange Galileo E5(E5a+E5b) I for Rinex3.

C8Q - org.orekit.gnss.ObservationType

Pseudorange Galileo E5(E5a+E5b) Q for Rinex3.

C8X - org.orekit.gnss.ObservationType

Pseudorange Galileo E5(E5a+E5b) I+Q for Rinex3.

C9A - org.orekit.gnss.ObservationType

Pseudorange IRNSS S A for Rinex3.

C9B - org.orekit.gnss.ObservationType

Pseudorange IRNSS S B for Rinex3.

C9C - org.orekit.gnss.ObservationType

Pseudorange IRNSS S C for Rinex3.

C9X - org.orekit.gnss.ObservationType

Pseudorange IRNSS S B+C for Rinex3.

CA - org.orekit.gnss.ObservationType

Pseudorange GPS L1 C/A / GLONASS G1 C/A for Rinex2.

CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential

Caching wrapper for NormalizedSphericalHarmonicsProvider.

CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Simple constructor.

calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.

canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Check if coefficients can be added.

CANNOT_FIND_SATELLITE_IN_SYSTEM - org.orekit.errors.OrekitMessages

CANNOT_PARSE_BOTH_TAU_AND_GAMMA - org.orekit.errors.OrekitMessages

CARRIER_PHASE - org.orekit.gnss.MeasurementType

Carrier-phase measurement.

CARRIER_POWER - org.orekit.files.ccsds.Keyword

Data: Carrier power [dBW].

CARTESIAN - org.orekit.orbits.OrbitType

Type for propagation in Cartesian parameters.

CartesianDerivativesFilter - Enum in org.orekit.utils

Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.

CartesianOrbit - Class in org.orekit.orbits

This class holds Cartesian orbital parameters.

CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from any kind of orbital parameters.

CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from Cartesian parameters.

CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from Cartesian parameters.

CB - org.orekit.gnss.ObservationType

Pseudorange GPS L1C for Rinex2.

CC - org.orekit.gnss.ObservationType

Pseudorange GPS L2C for Rinex2.

CCSDS_DATE_INVALID_LENGTH_TIME_FIELD - org.orekit.errors.OrekitMessages

CCSDS_DATE_INVALID_PREAMBLE_FIELD - org.orekit.errors.OrekitMessages

CCSDS_DATE_MISSING_AGENCY_EPOCH - org.orekit.errors.OrekitMessages

CCSDS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).

CCSDS_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01.

CCSDS_INVALID_FRAME - org.orekit.errors.OrekitMessages

CCSDS_NO_CORRESPONDING_TIME_SCALE - org.orekit.errors.OrekitMessages

CCSDS_OEM_INCONSISTENT_TIME_SYSTEMS - org.orekit.errors.OrekitMessages

CCSDS_OEM_VERS - org.orekit.files.ccsds.Keyword

File creation date in UTC.

CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.OEMWriter

Version number implemented.

CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.StreamingOemWriter

Version number implemented.

CCSDS_OMM_VERS - org.orekit.files.ccsds.Keyword

CCSDS OMM format version.

CCSDS_OPM_VERS - org.orekit.files.ccsds.Keyword

CCSDS OPM format version.

CCSDS_TDM_INCONSISTENT_DATA_LINE - org.orekit.errors.OrekitMessages

CCSDS_TDM_INCONSISTENT_TIME_SYSTEMS - org.orekit.errors.OrekitMessages

CCSDS_TDM_KEYWORD_NOT_FOUND - org.orekit.errors.OrekitMessages

CCSDS_TDM_UNKNOWN_FORMAT - org.orekit.errors.OrekitMessages

CCSDS_TDM_VERS - org.orekit.files.ccsds.Keyword

Header: TDM format version in the form of ‘x.y’, where ‘y’ shall be incremented for corrections and minor changes, and ‘x’ shall be incremented for major changes.

CCSDS_TDM_XML_INCONSISTENT_DATA_BLOCK - org.orekit.errors.OrekitMessages

CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED - org.orekit.errors.OrekitMessages

CCSDS_TIME_SYSTEM_NOT_READ_YET - org.orekit.errors.OrekitMessages

CCSDS_UNEXPECTED_KEYWORD - org.orekit.errors.OrekitMessages

CCSDS_UNKNOWN_CONVENTIONS - org.orekit.errors.OrekitMessages

CCSDS_UNKNOWN_GM - org.orekit.errors.OrekitMessages

CCSDS_UNKNOWN_SPACECRAFT_MASS - org.orekit.errors.OrekitMessages

CCSDSFrame - Enum in org.orekit.files.ccsds

Frames used in CCSDS Orbit Data Messages.

CcsdsModifiedFrame - Class in org.orekit.files.ccsds

A reference frame created from the REF_FRAME and CENTER_NAME is a CCSDS OPM, OMM, or OEM file.

CcsdsTimeScale - Enum in org.orekit.files.ccsds

The set of time scales defined in Annex A of the ODM CCSDS standard 502.0-B-2.

CD - org.orekit.gnss.ObservationType

Pseudorange GLONASS G2 for Rinex2.

CelestialBody - Interface in org.orekit.bodies

Interface for celestial bodies like Sun, Moon or solar system planets.

CelestialBodyFactory - Class in org.orekit.bodies

Factory class for bodies of the solar system.

CelestialBodyLoader - Interface in org.orekit.bodies

Interface for loading celestial bodies.

CelestialBodyPointed - Class in org.orekit.attitudes

This class handles a celestial body pointed attitude provider.

CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed

Creates new instance.

CENTER_NAME - org.orekit.files.ccsds.Keyword

Origin of reference frame.

CenterName - Enum in org.orekit.files.ccsds

Orbit central bodies for which a Celestial body can be created.

CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.forces.gravity.NewtonianAttraction

Name of the single parameter of this model: the central attraction coefficient.

checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory

Check Earth orientation parameters continuity.

checkTimeSystems() - Method in class org.orekit.files.ccsds.TDMFile

Check that, according to the CCSDS standard, every ObservationsBlock has the same time system.

ChronologicalComparator - Class in org.orekit.time

Comparator for TimeStamped instance.

ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator

Simple constructor.

CIRCULAR - org.orekit.orbits.OrbitType

Type for propagation in circular parameters.

CircularFieldOfViewDetector - Class in org.orekit.propagation.events

Finder for target entry/exit events with respect to a satellite sensor Field Of View.

CircularFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, double) - Constructor for class org.orekit.propagation.events.CircularFieldOfViewDetector

Build a new instance.

CircularOrbit - Class in org.orekit.orbits

This class handles circular orbital parameters.

CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit

Creates a new instance.

CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit

Creates a new instance.

CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from any kind of orbital parameters.

CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from Cartesian parameters.

CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from Cartesian parameters.

circularToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldCircularOrbit

Deprecated.

as of 9.3, replaced by FieldCircularOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) and FieldOrbit.getPVCoordinates()

CIRF_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined

CIRF frame, IERS 1996 conventions, with accurate EOP interpolation.

CIRF_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined

CIRF frame, IERS 1996 conventions, with simple EOP interpolation.

CIRF_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined

CIRF frame, IERS 2003 conventions, with accurate EOP interpolation.

CIRF_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined

CIRF frame, IERS 2003 conventions, with simple EOP interpolation.

CIRF_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined

CIRF frame, IERS 2010 conventions, with accurate EOP interpolation.

CIRF_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined

CIRF frame, IERS 2010 conventions, with simple EOP interpolation.

CIVIL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector

Sun elevation at civil dawn/dusk (6° below horizon).

CjSjCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the S_j(k, h) and the C_j(k, h) series and their partial derivatives with respect to k and h.

CjSjCoefficient(double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

C_j(k, h) and S_j(k, h) constructor.

ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for ClassicalRungeKuttaIntegrator.

ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder

Build a new instance.

CLASSIFICATION_TYPE - org.orekit.files.ccsds.Keyword

Classification type.

ClasspathCrawler - Class in org.orekit.data

Provider for data files stored as resources in the classpath.

ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler

Build a data classpath crawler.

ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler

Build a data classpath crawler.

clear() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue

Clear all stored events.

clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear all loaded celestial bodies.

clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear the specified celestial body from the internal cache.

clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear loaders for all celestial bodies.

clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear loaders for one celestial body.

clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory

Clear loaders for Earth Orientation Parameters history.

clearEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.FieldAbstractPropagator

Remove all events detectors.

clearEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Remove all events detectors.

clearEventsDetectors() - Method in interface org.orekit.propagation.Propagator

Remove all events detectors.

clearFilters() - Method in class org.orekit.data.DataProvidersManager

Remove all data filters, except the predefined ones.

clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Clear the recorded values from the interpolation grid.

clearLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager

Clear the set of data file names that have been loaded.

clearLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger

Clear the logged events.

clearLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger

Clear the logged events.

clearOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Clear ocean tides readers.

clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Clear gravity field readers.

clearProviders() - Method in class org.orekit.data.DataProvidersManager

Remove all data providers.

clearUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory

Clear loaders for UTC-TAI offsets history files.

CLOCK_BIAS - org.orekit.files.ccsds.Keyword

Data: Clock bias [s].

CLOCK_CORRECTIONS - Static variable in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider

Name of the additional state for satellite clock corrections.

CLOCK_DRIFT - org.orekit.files.ccsds.Keyword

Data: Clock drift [s/s].

CLOCK_OFFSET_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite

Prefix for clock offset parameter driver, the propagator index will be appended to it.

ClockCorrectionsProvider - Class in org.orekit.propagation.analytical.gnss

Provider for clock corrections as additional states.

ClockCorrectionsProvider(GPSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider

Simple constructor.

co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

C / (2 * A * B) .

coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

coef for SGP C3 computation.

coef1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

coef for SGP C5 computation.

CoefficientsFactory - Class in org.orekit.propagation.semianalytical.dsst.utilities

This class is designed to provide coefficient from the DSST theory.

CoefficientsFactory.NSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities

Key formed by two integer values.

COMMENT - org.orekit.files.ccsds.Keyword

Comments specific to a ODM file.

ComparableMeasurement - Interface in org.orekit.estimation.measurements

Base interface for comparing measurements regardless of their type.

compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator

Compare two time-stamped instances.

compareTo(ComparableMeasurement) - Method in interface org.orekit.estimation.measurements.ComparableMeasurement

compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate

Compare the instance with another date.

compareTo(DateComponents) - Method in class org.orekit.time.DateComponents

compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents

compareTo(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Compare the instance with another date.

compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents

COMPASS - org.orekit.files.sp3.SP3File.SP3FileType

COMPASS only file.

compile(PoissonSeries...) - Static method in class org.orekit.data.PoissonSeries

Join several nutation series, for fast simultaneous evaluation.

complainIfNotSupported(String) - Method in class org.orekit.forces.AbstractForceModel

Complain if a parameter is not supported.

compute(AbsoluteDate, List<Propagator>) - Method in class org.orekit.gnss.DOPComputer

Compute the DOP at a given date for a set of GNSS spacecrafts.

computeDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations

Compute differential equations for main state.

computeDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations

Compute the derivatives related to the additional state parameters.

computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations

Compute differential equations for main state.

computeDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.propagation.integration.AdditionalEquations

Compute the derivatives related to the additional state parameters.

computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Compute the derivatives related to the additional state parameters.

computeGsHs(double, double, double, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute recursively G_s and H_s polynomials from equation 3.1-(5).

computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Compute the roots for the Hansen coefficients and their derivatives.

computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the values for the first four coefficients and their derivatives by means of series.

computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Compute the initial values (see Collins, 4-255, 4-256 and 4.259)

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame

Compute the limit visibility point for a satellite in a given direction.

computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Conversion from osculating to mean orbit.

computeOsculatingState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Conversion from mean to osculating orbit.

computeQns(double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute the Q_n,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).

computeVns(int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute the V_n,s coefficients from 2.8.2-(1)(2).

computeZenithDelay(double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.DiscreteTroposphericModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.EstimatedTroposphericModel

This method allows the computation of the zenith hydrostatic and zenith total delays.

computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.MendesPavlisModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.TroposphericModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaOneModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaThreeModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.DiscreteTroposphericModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.EstimatedTroposphericModel

This method allows the computation of the zenith hydrostatic and zenith total delays.

computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.MendesPavlisModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.TroposphericModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaOneModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaThreeModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Configure ocean load deformation coefficients.

ConstantAzimuthAiming - Class in org.orekit.models.earth.tessellation

Class used to orient tiles with respect to a geographic azimuth.

ConstantAzimuthAiming(OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.tessellation.ConstantAzimuthAiming

Simple constructor.

ConstantProcessNoise - Class in org.orekit.estimation.sequential

Provider for constant process noise matrices.

ConstantProcessNoise(RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise

Simple constructor.

ConstantProcessNoise(RealMatrix, RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise

Simple constructor.

Constants - Interface in org.orekit.utils

Set of useful physical constants.

ConstantThrustManeuver - Class in org.orekit.forces.maneuvers

This class implements a simple maneuver with constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

contains(String) - Static method in enum org.orekit.files.ccsds.CcsdsTimeScale

Check if timeScale is one of the values supported by this enum.

containsSatellite(String) - Method in class org.orekit.files.sp3.SP3File

Tests whether a satellite with the given id is contained in this orbit file.

CONTINUE - org.orekit.propagation.events.handlers.EventHandler.Action

Continue indicator.

CONTINUE - org.orekit.propagation.events.handlers.FieldEventHandler.Action

Continue indicator.

ContinueOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Event handler which will always return continue as a state.

ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent

ContinuousScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation

Scheduler generating measurements sequences continuously.

ContinuousScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.ContinuousScheduler

Simple constructor.

convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter

Convert an osculating orbit into a mean orbit, in DSST sense.

convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter

Convert a row.

convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(List<SpacecraftState>, boolean, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(List<SpacecraftState>, boolean, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Convert a propagator to another.

convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Convert a propagator into another one.

convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Convert a propagator to another.

convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Convert a propagator into another one.

convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType

Convert an orbit to the instance type.

convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType

Convert an orbit to the instance type.

copy() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Create a copy of a NumericalPropagatorBuilder object.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouGeo

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouMeo

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Galileo

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GenericGNSS

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Glonass

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIA

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIF

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIR

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouGeo

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouMeo

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Galileo

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GenericGNSS

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Glonass

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIA

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIF

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIR

Compute GNSS attitude with midnight/noon yaw turn correction.

CORRECTION_ANGLE_1 - org.orekit.files.ccsds.Keyword

Meta-data: Correction angle 1.

CORRECTION_ANGLE_2 - org.orekit.files.ccsds.Keyword

Meta-data: Correction angle 2.

CORRECTION_DOPPLER - org.orekit.files.ccsds.Keyword

Meta-data: Correction Doppler.

CORRECTION_RANGE - org.orekit.files.ccsds.Keyword

Meta-data: Correction Range.

CORRECTION_RECEIVE - org.orekit.files.ccsds.Keyword

Meta-data: Correction receive.

CORRECTION_TRANSMIT - org.orekit.files.ccsds.Keyword

Meta-data: Correction transmit.

CORRECTIONS_APPLIED - org.orekit.files.ccsds.Keyword

Meta-data: Correction applied ? YES/NO

CORRUPTED_FILE - org.orekit.errors.OrekitMessages

cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

cosinus original inclination.

COV_REF_FRAME - org.orekit.files.ccsds.Keyword

Coordinate system for covariance matrix.

COVARIANCE_START - org.orekit.files.ccsds.Keyword

This keyword must appear before the first line of the covariance matrix data.

COVARIANCE_STOP - org.orekit.files.ccsds.Keyword

This keyword must appear after the last line of the covariance matrix data.

CovarianceMatrixProvider - Interface in org.orekit.estimation.sequential

Provider for process noise matrices.

create(double, double, int, EventHandler<? super ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

create(double, double, int, EventHandler<? super AlignmentDetector>) - Method in class org.orekit.propagation.events.AlignmentDetector

Build a new instance.

create(double, double, int, EventHandler<? super AltitudeDetector>) - Method in class org.orekit.propagation.events.AltitudeDetector

Build a new instance.

create(double, double, int, EventHandler<? super AngularSeparationDetector>) - Method in class org.orekit.propagation.events.AngularSeparationDetector

Build a new instance.

create(double, double, int, EventHandler<? super ApsideDetector>) - Method in class org.orekit.propagation.events.ApsideDetector

Build a new instance.

create(double, double, int, EventHandler<? super BooleanDetector>) - Method in class org.orekit.propagation.events.BooleanDetector

create(double, double, int, EventHandler<? super CircularFieldOfViewDetector>) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector

Build a new instance.

create(double, double, int, EventHandler<? super DateDetector>) - Method in class org.orekit.propagation.events.DateDetector

Build a new instance.

create(double, double, int, EventHandler<? super EclipseDetector>) - Method in class org.orekit.propagation.events.EclipseDetector

Build a new instance.

create(double, double, int, EventHandler<? super ElevationDetector>) - Method in class org.orekit.propagation.events.ElevationDetector

Build a new instance.

create(double, double, int, EventHandler<? super ElevationExtremumDetector>) - Method in class org.orekit.propagation.events.ElevationExtremumDetector

Build a new instance.

create(double, double, int, EventHandler<? super EventEnablingPredicateFilter<T>>) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter

Build a new instance.

create(double, double, int, EventHandler<? super EventShifter<T>>) - Method in class org.orekit.propagation.events.EventShifter

Build a new instance.

create(double, double, int, EventHandler<? super EventSlopeFilter<T>>) - Method in class org.orekit.propagation.events.EventSlopeFilter

Build a new instance.

create(double, double, int, EventHandler<? super FieldOfViewDetector>) - Method in class org.orekit.propagation.events.FieldOfViewDetector

Build a new instance.

create(double, double, int, EventHandler<? super FootprintOverlapDetector>) - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Build a new instance.

create(double, double, int, EventHandler<? super FunctionalDetector>) - Method in class org.orekit.propagation.events.FunctionalDetector

create(double, double, int, EventHandler<? super GeographicZoneDetector>) - Method in class org.orekit.propagation.events.GeographicZoneDetector

Build a new instance.

create(double, double, int, EventHandler<? super GroundAtNightDetector>) - Method in class org.orekit.propagation.events.GroundAtNightDetector

Build a new instance.

create(double, double, int, EventHandler<? super GroundFieldOfViewDetector>) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector

Build a new instance.

create(double, double, int, EventHandler<? super InterSatDirectViewDetector>) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Build a new instance.

create(double, double, int, EventHandler<? super LatitudeCrossingDetector>) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector

Build a new instance.

create(double, double, int, EventHandler<? super LatitudeExtremumDetector>) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector

Build a new instance.

create(double, double, int, EventHandler<? super LongitudeCrossingDetector>) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Build a new instance.

create(double, double, int, EventHandler<? super LongitudeExtremumDetector>) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector

Build a new instance.

create(double, double, int, EventHandler<? super NegateDetector>) - Method in class org.orekit.propagation.events.NegateDetector

create(double, double, int, EventHandler<? super NodeDetector>) - Method in class org.orekit.propagation.events.NodeDetector

Build a new instance.

create(double, double, int, EventHandler<? super PositionAngleDetector>) - Method in class org.orekit.propagation.events.PositionAngleDetector

Build a new instance.

create(double, double, int, EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector

Build a new instance.

create(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer

Creates a DOP computer for one location.

create(T, T, int, FieldEventHandler<? super D, T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Build a new instance.

create(T, T, int, FieldEventHandler<? super FieldAltitudeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector

Build a new instance.

create(T, T, int, FieldEventHandler<? super FieldApsideDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldApsideDetector

Build a new instance.

create(T, T, int, FieldEventHandler<? super FieldDateDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldDateDetector

Build a new instance.

create(T, T, int, FieldEventHandler<? super FieldEclipseDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector

Build a new instance.

create(T, T, int, FieldEventHandler<? super FieldElevationDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldElevationDetector

Build a new instance.

create(T, T, int, FieldEventHandler<? super FieldNodeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldNodeDetector

Build a new instance.

createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Besselian Epoch (BE).

createBesselianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Besselian Epoch (BE).

createFromModifiedRodrigues(double[][]) - Static method in class org.orekit.utils.AngularCoordinates

Convert a modified Rodrigues vector and derivatives to angular coordinates.

createFromModifiedRodrigues(T[][]) - Static method in class org.orekit.utils.FieldAngularCoordinates

Convert a modified Rodrigues vector and derivatives to angular coordinates.

createFromWeekComponents(int, int, int) - Static method in class org.orekit.time.DateComponents

Build a date from week components.

createGPSDate(int, double) - Static method in class org.orekit.time.AbsoluteDate

Deprecated.

as of 9.3, replaced by GPSDate(int, double).GPSDate.getDate()

createGPSDate(int, T) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a GPS date.

createInitialOrbit() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Build an initial orbit using the current selected parameters.

createJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Julian Day date.

createJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Julian Day date.

createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Julian Epoch (JE).

createJulianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Julian Epoch (JE).

createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Create a mapper between raw double components and spacecraft state.

createMJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Modified Julian Day date.

createMJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Modified Julian Day date.

createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Create an ITRF frame by transforming another ITRF frame.

CREATION_DATE - org.orekit.files.ccsds.Keyword

CCSDS OEM format version.

crossProduct(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldPVCoordinates

Compute the cross-product of two instances.

crossProduct(PVCoordinates, PVCoordinates) - Static method in class org.orekit.utils.PVCoordinates

Compute the cross-product of two instances.

CX_DOT_X - org.orekit.files.ccsds.Keyword

Covariance matrix [4, 1] element.

CX_DOT_X_DOT - org.orekit.files.ccsds.Keyword

Covariance matrix [4, 4] element.

CX_DOT_Y - org.orekit.files.ccsds.Keyword

Covariance matrix [4, 2] element.

CX_DOT_Z - org.orekit.files.ccsds.Keyword

Covariance matrix [4, 3] element.

CX_X - org.orekit.files.ccsds.Keyword

Covariance matrix [1, 1] element.

CY_DOT_X - org.orekit.files.ccsds.Keyword

Covariance matrix [5, 1] element.

CY_DOT_X_DOT - org.orekit.files.ccsds.Keyword

Covariance matrix [5, 4] element.

CY_DOT_Y - org.orekit.files.ccsds.Keyword

Covariance matrix [5, 2] element.

CY_DOT_Y_DOT - org.orekit.files.ccsds.Keyword

Covariance matrix [5, 5] element.

CY_DOT_Z - org.orekit.files.ccsds.Keyword

Covariance matrix [5, 3] element.

CY_X - org.orekit.files.ccsds.Keyword

Covariance matrix [2, 1] element.

CY_Y - org.orekit.files.ccsds.Keyword

Covariance matrix [2, 2] element.

CZ_DOT_X - org.orekit.files.ccsds.Keyword

Covariance matrix [6, 1] element.

CZ_DOT_X_DOT - org.orekit.files.ccsds.Keyword

Covariance matrix [6, 4] element.

CZ_DOT_Y - org.orekit.files.ccsds.Keyword

Covariance matrix [6, 2] element.

CZ_DOT_Y_DOT - org.orekit.files.ccsds.Keyword

Covariance matrix [6, 5] element.

CZ_DOT_Z - org.orekit.files.ccsds.Keyword

Covariance matrix [6, 3] element.

CZ_DOT_Z_DOT - org.orekit.files.ccsds.Keyword

Covariance matrix [6, 6] element.

CZ_X - org.orekit.files.ccsds.Keyword

Covariance matrix [3, 1] element.

CZ_Y - org.orekit.files.ccsds.Keyword

Covariance matrix [3, 2] element.

CZ_Z - org.orekit.files.ccsds.Keyword

Covariance matrix [3, 3] element.

D

D1 - org.orekit.gnss.ObservationType

Doppler GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.

D1A - org.orekit.gnss.ObservationType

Doppler Galileo E1 A for Rinex3.

D1B - org.orekit.gnss.ObservationType

Doppler Galileo E1 I/NAV OS/CS/SoL for Rinex3.

D1C - org.orekit.gnss.ObservationType

Doppler GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.

D1I - org.orekit.gnss.ObservationType

Doppler Beidou B1 I for Rinex3.

D1L - org.orekit.gnss.ObservationType

Doppler GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3.

D1M - org.orekit.gnss.ObservationType

Doppler GPS L2 M for Rinex3.

D1N - org.orekit.gnss.ObservationType

Doppler GPS L1 codeless for Rinex3.

D1P - org.orekit.gnss.ObservationType

Doppler GPS L2 P(AS off) / GLONASS G2 P for Rinex3.

D1S - org.orekit.gnss.ObservationType

Doppler GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3.

D1W - org.orekit.gnss.ObservationType

Doppler GPS L1 Z-tracking and similar (AS on) for Rinex3.

D1X - org.orekit.gnss.ObservationType

Doppler GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) for Rinex3.

D1Y - org.orekit.gnss.ObservationType

Doppler GPS L1 Y for Rinex3.

D1Z - org.orekit.gnss.ObservationType

Doppler Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3.

D2 - org.orekit.gnss.ObservationType

Doppler GPS L2 / GLONASS G2 / Beidou BO2 for Rinex2.

D2C - org.orekit.gnss.ObservationType

Doppler GPS L2 C/A / GLONASS G2 C/A for Rinex3.

D2D - org.orekit.gnss.ObservationType

Doppler GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.

D2I - org.orekit.gnss.ObservationType

Doppler Beidou B1 I for Rinex3.03.

D2L - org.orekit.gnss.ObservationType

Doppler GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.

D2M - org.orekit.gnss.ObservationType

Doppler GPS L2 M for Rinex3.

D2N - org.orekit.gnss.ObservationType

Doppler GPS L2 codeless for Rinex3.

D2P - org.orekit.gnss.ObservationType

Doppler GPS L2 P(AS off) / GLONASS G2 P for Rinex3.

D2Q - org.orekit.gnss.ObservationType

Doppler Beidou B1 Q for Rinex3.03.

D2S - org.orekit.gnss.ObservationType

Doppler GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.

D2W - org.orekit.gnss.ObservationType

Doppler GPS L2 Z-tracking and similar (AS on) for Rinex3.

D2X - org.orekit.gnss.ObservationType

Doppler GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3.

D2Y - org.orekit.gnss.ObservationType

Doppler GPS L2 Y for Rinex3.

D3I - org.orekit.gnss.ObservationType

Doppler GLONASS G3 I for Rinex3.

D3Q - org.orekit.gnss.ObservationType

Doppler GLONASS G3 Q for Rinex3.

D3X - org.orekit.gnss.ObservationType

Doppler GLONASS G3 I+Q for Rinex3.

D5 - org.orekit.gnss.ObservationType

Doppler GPS L5 / Galileo E5a / SBAS L5 for Rinex2.

D5A - org.orekit.gnss.ObservationType

Doppler IRNSS L5 A for Rinex3.

D5B - org.orekit.gnss.ObservationType

Doppler IRNSS L5 B for Rinex3.

D5C - org.orekit.gnss.ObservationType

Doppler IRNSS L5 C for Rinex3.

D5I - org.orekit.gnss.ObservationType

Doppler GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.

D5Q - org.orekit.gnss.ObservationType

Doppler GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.

D5X - org.orekit.gnss.ObservationType

Doppler GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C for Rinex3.

D6 - org.orekit.gnss.ObservationType

Doppler Galileo E6 / Beidou B03 for Rinex2.

D6A - org.orekit.gnss.ObservationType

Doppler Galileo E6 A PRS for Rinex3.

D6B - org.orekit.gnss.ObservationType

Doppler Galileo E6 B C/NAV CS for Rinex3.

D6C - org.orekit.gnss.ObservationType

Doppler Galileo E6 C no data for Rinex3.

D6I - org.orekit.gnss.ObservationType

Doppler Beidou B3 I for Rinex3.

D6L - org.orekit.gnss.ObservationType

Doppler QZSS LEX(6) L for Rinex3.

D6Q - org.orekit.gnss.ObservationType

Doppler Beidou B3 Q for Rinex3.

D6S - org.orekit.gnss.ObservationType

Doppler QZSS LEX(6) S for Rinex3.

D6X - org.orekit.gnss.ObservationType

Doppler Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q for Rinex3.

D6Z - org.orekit.gnss.ObservationType

Doppler Galileo E6 A+B+C for Rinex3.

D7 - org.orekit.gnss.ObservationType

Doppler Galileo E5b / Beidou B02 for Rinex2.

D7I - org.orekit.gnss.ObservationType

Doppler Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.

D7Q - org.orekit.gnss.ObservationType

Doppler Galileo Q no data / Beidou B2 Q for Rinex3.

D7X - org.orekit.gnss.ObservationType

Doppler Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.

D8 - org.orekit.gnss.ObservationType

Doppler Galileo E5a+b for Rinex2.

D8I - org.orekit.gnss.ObservationType

Doppler Galileo E5(E5a+E5b) I for Rinex3.

D8Q - org.orekit.gnss.ObservationType

Doppler Galileo E5(E5a+E5b) Q for Rinex3.

D8X - org.orekit.gnss.ObservationType

Doppler Galileo E5(E5a+E5b) I+Q for Rinex3.

D9A - org.orekit.gnss.ObservationType

Doppler IRNSS S A for Rinex3.

D9B - org.orekit.gnss.ObservationType

Doppler IRNSS S B for Rinex3.

D9C - org.orekit.gnss.ObservationType

Doppler IRNSS S C for Rinex3.

D9X - org.orekit.gnss.ObservationType

Doppler IRNSS S B+C for Rinex3.

DA - org.orekit.gnss.ObservationType

Doppler GPS L1 C/A / GLONASS G1 C/A for Rinex2.

data - org.orekit.files.ccsds.Keyword

Data keyword.

DATA_QUALITY - org.orekit.files.ccsds.Keyword

Meta-data: Data quality.

DATA_ROOT_DIRECTORY_DOES_NOT_EXIST - org.orekit.errors.OrekitMessages

DATA_START - org.orekit.files.ccsds.Keyword

Keyword used to delineate the start of a Data block in Keyvalue files.

DATA_STOP - org.orekit.files.ccsds.Keyword

Keyword used to delineate the end of a Data block in Keyvalue files..

DataFilter - Interface in org.orekit.data

Interface for filtering data (typically uncompressing it) in data providers before passing it to data loaders.

DataLoader - Interface in org.orekit.data

Interface for loading data files from data providers.

DataProvider - Interface in org.orekit.data

Interface for providing data files to file loaders.

DataProvidersManager - Class in org.orekit.data

Singleton class managing all supported data providers.

DateComponents - Class in org.orekit.time

Class representing a date broken up as year, month and day components.

DateComponents(int) - Constructor for class org.orekit.time.DateComponents

Build a date from its offset with respect to a DateComponents.J2000_EPOCH.

DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents

Build a date from a year and day number.

DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its components.

DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its components.

DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its offset with respect to a reference epoch.

DateDetector - Class in org.orekit.propagation.events

Finder for date events.

DateDetector(double, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector

Build a new instance.

DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector

Build a new instance.

DatesSelector - Interface in org.orekit.time

Interface for selecting dates within an interval.

DateTimeComponents - Class in org.orekit.time

Holder for date and time components.

DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents

Build a new instance from its components.

DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from a seconds offset with respect to another one.

DB - org.orekit.gnss.ObservationType

Doppler GPS L1C for Rinex2.

DC - org.orekit.gnss.ObservationType

Doppler GPS L2C for Rinex2.

DD - org.orekit.gnss.ObservationType

Doppler GLONASS G2 for Rinex2.

DECEMBER - org.orekit.time.Month

December.

decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Configure the matrix decomposer.

deepPeriodicEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4

Computes periodic terms from current coordinates and epoch.

DeepSDP4 - Class in org.orekit.propagation.analytical.tle

This class contains the methods that compute deep space perturbation terms.

DeepSDP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.DeepSDP4

Constructor for a unique initial TLE.

deepSecularEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4

Computes secular terms from current coordinates and epoch.

DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for default type of ephemeris (SGP4/SDP4).

DEFAULT_ANTEX_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.antenna.AntexLoader

Default supported files name pattern for antex files.

DEFAULT_BLQ_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

Default supported files name pattern for Onsala Space Observatory files in BLQ format.

DEFAULT_CACHED_SLOTS_NUMBER - Static variable in class org.orekit.utils.GenericTimeStampedCache

Default number of independent cached time slots.

DEFAULT_CORRECTION_FACTOR - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default correction factor value.

DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader

Default supported files name pattern for JPL DE files.

DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.propagation.analytical.Ephemeris

Default extrapolation time threshold: 1ms.

DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader

Default supported files name pattern for IMCCE INPOP files.

DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.ccsds.OEMWriter

Default interpolation method if the user specifies none.

DEFAULT_INTERPOLATION_SIZE - Static variable in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Defines the default interpolation sample size if it is not specified on a segment.

DEFAULT_LAW - Static variable in interface org.orekit.propagation.FieldPropagator

Default attitude provider.

DEFAULT_LAW - Static variable in interface org.orekit.propagation.Propagator

Default attitude provider.

DEFAULT_MASS - Static variable in interface org.orekit.propagation.FieldPropagator

Default mass.

DEFAULT_MASS - Static variable in interface org.orekit.propagation.Propagator

Default mass.

DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.AbstractDetector

Default cmaximum number of iterations in the event time search.

DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldAbstractDetector

Default cmaximum number of iterations in the event time search.

DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector

Default maximum checking interval (s).

DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.FieldAbstractDetector

Default maximum checking interval (s).

DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.OEMWriter

Default originator field value if user specifies none.

DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.StreamingOemWriter

Default value for Keyword.ORIGINATOR.

DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.OceanTides

Default number of points tides field sampling.

DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.SolidTides

Default number of points tides field sampling.

DEFAULT_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default local pressure at viewpoint (Pa).

DEFAULT_RINEX_2_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.RinexLoader

Default supported files name pattern for rinex 2 observation files.

DEFAULT_RINEX_3_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.RinexLoader

Default supported files name pattern for rinex 3 observation files.

DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.OceanTides

Default step for tides field sampling (seconds).

DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.SolidTides

Default step for tides field sampling (seconds).

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.GlobalPressureTemperature2Model

Default supported files name pattern.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Default supported files name pattern.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.ViennaModelCoefficientsLoader

Default supported files name pattern.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.TAIUTCDatFilesLoader

Default supported files name pattern.

DEFAULT_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default local temperature at viewpoint (K).

DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector

Default convergence threshold (s).

DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldAbstractDetector

Default convergence threshold (s).

DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIA

Default yaw bias (rad).

DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF

Default yaw bias (rad).

DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Galileo

Default yaw rates for all spacecrafts in radians per seconds.

DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Glonass

Default yaw rates for all spacecrafts in radians per seconds.

DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF

Default yaw rates for all spacecrafts in radians per seconds.

DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIR

Default yaw rates for all spacecrafts in radians per seconds.

DEFAULT_YAW_RATES - Static variable in class org.orekit.gnss.attitude.GPSBlockIIA

Default yaw rates for all spacecrafts in radians per seconds (indexed by prnNumber, hence entry 0 is unused).

DEGREES - org.orekit.data.PolynomialParser.Unit

Degrees angles.

DelaunayArguments - Class in org.orekit.data

Delaunay arguments used for nutation or tides.

DelaunayArguments(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments

Simple constructor.

DELTA_R_FILE_NAME - Static variable in class org.orekit.models.earth.SaastamoinenModel

Default file name for δR correction term table.

dependsOnPositionOnly() - Method in class org.orekit.forces.drag.DragForce

Check if force models depends on position only.

dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModel

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.NewtonianAttraction

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.OceanTides

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.Relativity

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SolidTides

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.HarmonicParametricAcceleration

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.PolynomialParametricAcceleration

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Check if force models depends on position only.

derivative(double) - Method in class org.orekit.data.PolynomialNutation

Evaluate the time derivative of the polynomial.

derivative(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate time derivative of a set of Poisson series.

derivative(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate time derivative of a set of Poisson series.

derivative(T) - Method in class org.orekit.data.PolynomialNutation

Evaluate the time derivative of the polynomial.

differentiate(ParameterFunction, int, double) - Static method in class org.orekit.utils.Differentiation

Differentiate a scalar function using finite differences.

differentiate(ParameterFunction, ParameterDriver, int, double) - Static method in class org.orekit.utils.Differentiation

Deprecated.

as of 9.3, replaced by Differentiation.differentiate(ParameterFunction, int, double)

differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngle, double, int) - Static method in class org.orekit.utils.Differentiation

Differentiate a vector function using finite differences.

Differentiation - Class in org.orekit.utils

Utility class for differentiating various kinds of functions.

DIMENSION_INCONSISTENT_WITH_PARAMETERS - org.orekit.errors.OrekitMessages

DirectoryCrawler - Class in org.orekit.data

Provider for data files stored in a directories tree on filesystem.

DirectoryCrawler(File) - Constructor for class org.orekit.data.DirectoryCrawler

Build a data files crawler.

DiscreteTroposphericModel - Interface in org.orekit.models.earth

Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.

displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.OceanLoading

Compute displacement of a ground reference point.

displacement(BodiesElements, Frame, Vector3D) - Method in interface org.orekit.models.earth.displacement.StationDisplacement

Compute displacement of a ground reference point.

displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.TidalDisplacement

Compute displacement of a ground reference point.

doEvent(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState

Notify the user's listener of the event.

doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState

Notify the user's listener of the event.

DOP - Class in org.orekit.gnss

This class is a container for the result of a single DOP computation.

DOP(GeodeticPoint, AbsoluteDate, int, double, double, double, double, double) - Constructor for class org.orekit.gnss.DOP

Constructor.

DOP_MIN_ELEVATION - Static variable in class org.orekit.gnss.DOPComputer

Minimum elevation : 0°.

DOPComputer - Class in org.orekit.gnss

This class aims at computing the dilution of precision.

DOPPLER - org.orekit.gnss.MeasurementType

Doppler measurement.

DOPPLER_INSTANTANEOUS - org.orekit.files.ccsds.Keyword

Data: Doppler instantaneous [km/s].

DOPPLER_INTEGRATED - org.orekit.files.ccsds.Keyword

Data: Doppler integrated [km/s].

DOR - org.orekit.files.ccsds.Keyword

Data: DOR [s].

DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for DormandPrince54Integrator.

DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder

Build a new instance.

DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for DormandPrince853Integrator.

DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder

Build a new instance.

DRAG_AREA - org.orekit.files.ccsds.Keyword

Drag area.

DRAG_COEFF - org.orekit.files.ccsds.Keyword

Drag coefficient.

DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive

Parameter name for drag coefficient enabling Jacobian processing.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to drag.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in interface org.orekit.forces.drag.DragSensitive

Compute the acceleration due to drag.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in class org.orekit.forces.drag.IsotropicDrag

Compute the acceleration due to drag.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute acceleration due to drag, with parameters derivatives.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String) - Method in interface org.orekit.forces.drag.DragSensitive

Compute acceleration due to drag, with parameters derivatives.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String) - Method in class org.orekit.forces.drag.IsotropicDrag

Compute acceleration due to drag, with parameters derivatives.

dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to drag.

dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.drag.DragSensitive

Compute the acceleration due to drag.

dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.drag.IsotropicDrag

Compute the acceleration due to drag.

DragForce - Class in org.orekit.forces.drag

Atmospheric drag force model.

DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce

Simple constructor.

DragSensitive - Interface in org.orekit.forces.drag

Interface for spacecraft that are sensitive to atmospheric drag forces.

DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD - org.orekit.errors.OrekitMessages

DSST_NEWCOMB_OPERATORS_COMPUTATION - org.orekit.errors.OrekitMessages

DSST_SPR_SHADOW_INCONSISTENT - org.orekit.errors.OrekitMessages

DSST_VMNS_COEFFICIENT_ERROR_MS - org.orekit.errors.OrekitMessages

DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces

Atmospheric drag contribution to the DSSTPropagator.

DSSTAtmosphericDrag(Atmosphere, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Simple constructor assuming spherical spacecraft.

DSSTAtmosphericDrag(Atmosphere, DragSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Simple constructor with custom spacecraft.

DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces

This interface represents a force modifying spacecraft motion for a DSSTPropagator.

DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst

This class propagates orbits using the DSST theory.

DSSTPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a new instance of DSSTPropagator.

DSSTPropagator(ODEIntegrator, boolean) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a new instance of DSSTPropagator.

DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces

Solar radiation pressure contribution to the DSSTPropagator.

DSSTSolarRadiationPressure(double, double, double, double, ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Constructor with customizable reference values but spherical spacecraft.

DSSTSolarRadiationPressure(double, double, double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Deprecated.

as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, double, double, ExtendedPVCoordinatesProvider, double)

DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Simple constructor with default reference values and spherical spacecraft.

DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Complete constructor.

DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Deprecated.

as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double)

DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Deprecated.

as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive)

DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Simple constructor with default reference values, but custom spacecraft.

DSSTSolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Deprecated.

as of 9.2 replaced by {DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive)

DSSTTesseral - Class in org.orekit.propagation.semianalytical.dsst.forces

Tesseral contribution to the central body gravitational perturbation.

DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider, int, int, int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Simple constructor.

DSSTThirdBody - Class in org.orekit.propagation.semianalytical.dsst.forces

Third body attraction perturbation to the DSSTPropagator.

DSSTThirdBody(CelestialBody) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Complete constructor.

DSSTZonal - Class in org.orekit.propagation.semianalytical.dsst.forces

Zonal contribution to the central body gravitational perturbation.

DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Simple constructor.

DTM2000 - Class in org.orekit.forces.drag.atmosphere

This atmosphere model is the realization of the DTM-2000 model.

DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.atmosphere.DTM2000

Simple constructor for independent computation.

DTM2000InputParameters - Interface in org.orekit.forces.drag.atmosphere

Container for solar activity data, compatible with DTM2000 Atmosphere model.

DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE - org.orekit.errors.OrekitMessages

durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate

Compute the physically elapsed duration between two instants.

durationFrom(AbsoluteDate) - Method in class org.orekit.time.FieldAbsoluteDate

Compute the physically elapsed duration between two instants.

durationFrom(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Compute the physically elapsed duration between two instants.

DynamicOutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers

Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.

DynamicOutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter

Simple constructor.

E

e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final eccentricity.

E01 - org.orekit.gnss.Frequency

Galileo, "E1" (1575.42 MHz).

E05 - org.orekit.gnss.Frequency

Galileo E5a (1176.45 MHz).

E06 - org.orekit.gnss.Frequency

Galileo E6 (1278.75 MHz).

E07 - org.orekit.gnss.Frequency

Galileo E5b (1207.14 MHz).

E08 - org.orekit.gnss.Frequency

Galileo E5 (E5a + E5b) (1191.795MHz).

e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original eccentricity squared.

EARTH - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for the Earth.

EARTH - org.orekit.files.ccsds.CenterName

Earth body.

EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Earth.

EARTH_ANGULAR_VELOCITY - Static variable in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Earth Angular Velocity, in rad/s, from TIRF model.

EARTH_MOON - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for the Earth-Moon barycenter.

EARTH_MOON - org.orekit.files.ccsds.CenterName

Earth-Moon barycenter bodies pair.

EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Earth-Moon barycenter.

EarthITU453AtmosphereRefraction - Class in org.orekit.models.earth

Implementation of refraction model for Earth exponential atmosphere based on ITU-R P.834-7 recommendation.

EarthITU453AtmosphereRefraction(double) - Constructor for class org.orekit.models.earth.EarthITU453AtmosphereRefraction

Creates a new default instance.

EarthShape - Interface in org.orekit.models.earth

All models of Earth's shape have some common properties that are not shared with arbitrary BodyShapes.

EarthStandardAtmosphereRefraction - Class in org.orekit.models.earth

Implementation of refraction model for Earth standard atmosphere.

EarthStandardAtmosphereRefraction() - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Creates a new default instance.

EarthStandardAtmosphereRefraction(double, double) - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Creates an instance given a specific pressure and temperature.

ecc - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Eccentricity.

ECCENTRIC - org.orekit.orbits.PositionAngle

Eccentric angle.

ECCENTRICITY - org.orekit.files.ccsds.Keyword

Orbit eccentricity.

eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit

Computes the mean latitude argument from the eccentric latitude argument.

eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit

Computes the mean longitude argument from the eccentric longitude argument.

eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Computes the mean latitude argument from the eccentric latitude argument.

eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Computes the mean longitude argument from the eccentric longitude argument.

eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit

Computes the true latitude argument from the eccentric latitude argument.

eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit

Computes the true longitude argument from the eccentric longitude argument.

eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Computes the true latitude argument from the eccentric latitude argument.

eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Computes the true longitude argument from the eccentric longitude argument.

ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder

Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.

eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder

Sets the Earth Centered Inertial frame used for propagation.

EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical

This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.

EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit and potential.

EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, mass and potential.

EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, mass and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider and potential.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Private helper constructor.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider and potential provider.

EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit and potential provider.

EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for Eckstein-Hechler propagator.

EcksteinHechlerPropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a new instance.

EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a new instance.

EclipseDetector - Class in org.orekit.propagation.events

Finder for satellite eclipse related events.

EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector

Build a new eclipse detector.

EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector

Build a new eclipse detector.

EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector

Build a new eclipse detector.

ECLIPTIC_CONVENTIONS_1996 - org.orekit.frames.Predefined

Ecliptic framen IERS 1996 conventions.

ECLIPTIC_CONVENTIONS_2003 - org.orekit.frames.Predefined

Ecliptic framen IERS 2003 conventions.

ECLIPTIC_CONVENTIONS_2010 - org.orekit.frames.Predefined

Ecliptic framen IERS 2010 conventions.

EclipticProvider - Class in org.orekit.frames

An inertial frame aligned with the ecliptic.

EclipticProvider(IERSConventions) - Constructor for class org.orekit.frames.EclipticProvider

Create a transform provider from MOD to an ecliptically aligned frame.

eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original eccentricity * eta.

EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for EGM files.

EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.

EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.

EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.

EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.

EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.

EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from EGM96 model: 6378136.3 m.

EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².

EGMFormatReader - Class in org.orekit.forces.gravity.potential

This reader is adapted to the EGM Format.

EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader

Simple constructor.

EGMFormatReader(String, boolean, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader

Simple constructor that allows overriding 'standard' EGM96 ae and mu with WGS84 variants.

EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.

EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.

EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.

EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.

EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.

EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from EIGEN5C model: 6378136.46 m.

EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².

ELEMENT_SET_NO - org.orekit.files.ccsds.Keyword

Element set number of the satellite.

ElevationDetector - Class in org.orekit.propagation.events

Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.

ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.

ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.

ElevationExtremumDetector - Class in org.orekit.propagation.events

Detector for elevation extremum with respect to a ground point.

ElevationExtremumDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector

Build a detector.

ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector

Build a new detector.

ElevationMask - Class in org.orekit.utils

Class for modeling the ground elevation values around a given point.

ElevationMask(double[][]) - Constructor for class org.orekit.utils.ElevationMask

Creates an instance of an Elevation mask based on the passed in parameter.

Ellipse - Class in org.orekit.bodies

Model of a 2D ellipse in 3D space.

Ellipse(Vector3D, Vector3D, Vector3D, double, double, Frame) - Constructor for class org.orekit.bodies.Ellipse

Simple constructor.

Ellipsoid - Class in org.orekit.bodies

Modeling of a general three-axes ellipsoid.

Ellipsoid(Frame, double, double, double) - Constructor for class org.orekit.bodies.Ellipsoid

Simple constructor.

EllipsoidTessellator - Class in org.orekit.models.earth.tessellation

Class used to tessellate an interest zone on an ellipsoid in either tiles or grids of geodetic points.

EllipsoidTessellator(OneAxisEllipsoid, TileAiming, int) - Constructor for class org.orekit.models.earth.tessellation.EllipsoidTessellator

Simple constructor.

ellipticEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit

Computes the mean anomaly from the elliptic eccentric anomaly.

ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Computes the mean anomaly from the elliptic eccentric anomaly.

ellipticEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit

Computes the true anomaly from the elliptic eccentric anomaly.

ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Computes the true anomaly from the elliptic eccentric anomaly.

ellipticKeplerianToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Deprecated.

as of 9.3 replaced with FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) and FieldOrbit.getPVCoordinates()

EME2000 - org.orekit.files.ccsds.CCSDSFrame

Earth Mean Equator and Equinox of J2000.

EME2000 - org.orekit.frames.Predefined

EME2000 frame.

EME2000_ALIGNED - Static variable in class org.orekit.attitudes.InertialProvider

Dummy attitude provider, perfectly aligned with the EME2000 frame.

emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache

Get an empty immutable cache, cast to the correct type.

EnablingPredicate<S extends EventDetector> - Interface in org.orekit.propagation.events

This interface represents an event enabling predicate function.

endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

End parsing.

ensureCompatibleAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldSpacecraftState

Check if two instances have the same set of additional states available.

ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState

Check if two instances have the same set of additional states available.

EOPBasedTransformProvider - Interface in org.orekit.frames

Interface for Transform providers that use Earth Orientation Parameters.

EOPC04_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the EOPC04 files (IAU1980 compatibles).

EOPC04_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the EOPC04 files (IAU2000 compatibles).

EOPEntry - Class in org.orekit.frames

This class holds an Earth Orientation Parameters entry.

EOPEntry(int, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.EOPEntry

Deprecated.

as of 9.2 replaced with EOPEntry(int, double, double, double, double, double, double, double, double, ITRFVersion)

EOPEntry(int, double, double, double, double, double, double, double, double, ITRFVersion) - Constructor for class org.orekit.frames.EOPEntry

Simple constructor.

EOPHistory - Class in org.orekit.frames

This class loads any kind of Earth Orientation Parameter data throughout a large time range.

EOPHistory(IERSConventions, Collection<EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory

Simple constructor.

EOPHistoryLoader - Interface in org.orekit.frames

Interface for loading Earth Orientation Parameters history.

EphemeridesBlock() - Constructor for class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

EphemeridesBlock constructor.

Ephemeris - Class in org.orekit.propagation.analytical

This class is designed to accept and handle tabulated orbital entries.

Ephemeris(List<SpacecraftState>, int) - Constructor for class org.orekit.propagation.analytical.Ephemeris

Constructor with tabulated states.

Ephemeris(List<SpacecraftState>, int, double) - Constructor for class org.orekit.propagation.analytical.Ephemeris

Constructor with tabulated states.

EPHEMERIS_FILE_NO_MULTI_SUPPORT - org.orekit.errors.OrekitMessages

EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.FieldPropagator

Indicator for ephemeris generation mode.

EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.Propagator

Indicator for ephemeris generation mode.

EPHEMERIS_TYPE - org.orekit.files.ccsds.Keyword

Ephemeris type.

EphemerisFile - Interface in org.orekit.files.general

An interface for accessing the data stored in an ephemeris file and using the data to create a working Propagator.

EphemerisFile.EphemerisSegment - Interface in org.orekit.files.general

A segment of an ephemeris for a satellite.

EphemerisFile.SatelliteEphemeris - Interface in org.orekit.files.general

Contains the information about a single satellite from an EphemerisFile.

EphemerisFileParser - Interface in org.orekit.files.general

Parse an ephemeris file.

EphemerisFileWriter - Interface in org.orekit.files.general

An interface for writing out ephemeris files to disk.

EPOCH - org.orekit.files.ccsds.Keyword

Epoch of state vector and optional Keplerian elements.

equals(Object) - Method in class org.orekit.bodies.FieldGeodeticPoint

equals(Object) - Method in class org.orekit.bodies.GeodeticPoint

equals(Object) - Method in class org.orekit.models.earth.displacement.Tide

equals(Object) - Method in class org.orekit.propagation.analytical.tle.TLE

Check if this tle equals the provided tle.

equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

equals(Object) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represent the same time as another instance.

equals(Object) - Method in class org.orekit.time.DateComponents

equals(Object) - Method in class org.orekit.time.DateTimeComponents

equals(Object) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represent the same time as another instance.

equals(Object) - Method in class org.orekit.time.TimeComponents

EQUINOCTIAL - org.orekit.orbits.OrbitType

Type for propagation in equinoctial parameters.

EquinoctialOrbit - Class in org.orekit.orbits

This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.

EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Creates a new instance.

EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Creates a new instance.

EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from any kind of orbital parameters.

EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from Cartesian parameters.

EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from Cartesian parameters.

equinoctialToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Deprecated.

as of 9.3, replaced by FieldEquinoctialOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) and FieldOrbit.getPVCoordinates()

estimate() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Estimate the orbital, propagation and measurements parameters.

estimate(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Estimate the theoretical value of the measurement.

estimate(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Estimate the theoretical value of the measurement.

estimate(Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double) - Method in class org.orekit.estimation.iod.IodGooding

Orbit got from Observed Three Lines of Sight (angles only).

estimate(Frame, boolean, int, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodLambert

Estimate a Keplerian orbit given two position vectors and a duration.

estimate(Frame, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodGibbs

Give an initial orbit estimation, assuming Keplerian motion.

estimate(Frame, PV, PV, PV) - Method in class org.orekit.estimation.iod.IodGibbs

Give an initial orbit estimation, assuming Keplerian motion.

EstimatedEarthFrameProvider - Class in org.orekit.estimation.measurements

Class modeling an Earth frame whose Earth Orientation Parameters can be estimated.

EstimatedEarthFrameProvider(UT1Scale) - Constructor for class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Build an estimated Earth frame.

EstimatedMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements

Class holding an estimated theoretical value associated to an observed measurement.

EstimatedMeasurement(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement

Simple constructor.

EstimatedMeasurement.Status - Enum in org.orekit.estimation.measurements

Enumerate for the status of the measurement.

estimatedMeasurementsParameters(ParameterDriversList) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Configure the estimated measurement parameters.

EstimatedTroposphericModel - Class in org.orekit.models.earth

An estimated tropospheric model.

EstimatedTroposphericModel(double, double, MappingFunction, double) - Constructor for class org.orekit.models.earth.EstimatedTroposphericModel

Build a new instance using the given environmental conditions.

EstimatedTroposphericModel(MappingFunction, double) - Constructor for class org.orekit.models.earth.EstimatedTroposphericModel

Build a new instance using a standard atmosphere model.

estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates

Estimate rotation rate between two orientations.

estimateRate(FieldRotation<T>, FieldRotation<T>, T) - Static method in class org.orekit.utils.FieldAngularCoordinates

Estimate rotation rate between two orientations.

estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates

Estimate rotation rate between two orientations.

estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates

Estimate velocity between two positions.

estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates

Estimate velocity between two positions.

EstimationModifier<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements

Interface for estimated measurements modifiers used for orbit determination.

EstimationsProvider - Interface in org.orekit.estimation.measurements

Interface for retrieving estimated measurements during orbit determination.

estimationStep(ObservedMeasurement<?>) - Method in class org.orekit.estimation.sequential.KalmanEstimator

Process a single measurement.

eta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

eta from SPTRCK #3.

etasq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

eta squared.

EulerIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for EulerIntegrator.

EulerIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerIntegratorBuilder

Build a new instance.

evaluateAll(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments

Evaluate all fundamental arguments for the current date (Delaunay plus planetary).

evaluateAll(FieldAbsoluteDate<T>) - Method in class org.orekit.data.FundamentalNutationArguments

Evaluate all fundamental arguments for the current date (Delaunay plus planetary).

evaluateStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState

Evaluate the impact of the proposed step on the event detector.

evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState

Evaluate the impact of the proposed step on the event detector.

evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions

Evaluate the date offset between the current date and the reference date.

evaluateTC(FieldAbsoluteDate<T>) - Method in enum org.orekit.utils.IERSConventions

Evaluate the date offset between the current date and the reference date.

evaluationPerformed(int, int, Orbit[], ParameterDriversList, ParameterDriversList, ParameterDriversList, EstimationsProvider, LeastSquaresProblem.Evaluation) - Method in interface org.orekit.estimation.leastsquares.BatchLSObserver

Notification callback for the end of each evaluation.

evaluationPerformed(KalmanEstimation) - Method in interface org.orekit.estimation.sequential.KalmanObserver

Notification callback after each one of a Kalman filter estimation.

EVENT_DATE_TOO_CLOSE - org.orekit.errors.OrekitMessages

EventBasedScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation

Scheduler based on EventDetector for generating measurements sequences.

EventBasedScheduler(MeasurementBuilder<T>, DatesSelector, Propagator, EventDetector, SignSemantic) - Constructor for class org.orekit.estimation.measurements.generation.EventBasedScheduler

Simple constructor.

EventDetector - Interface in org.orekit.propagation.events

This interface represents space-dynamics aware events detectors.

EventEnablingPredicateFilter<T extends EventDetector> - Class in org.orekit.propagation.events

Wrapper used to detect events only when enabled by an external predicated function.

EventEnablingPredicateFilter(T, EnablingPredicate<? super T>) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter

Wrap an event detector.

EventHandler<T extends EventDetector> - Interface in org.orekit.propagation.events.handlers

An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.

EventHandler.Action - Enum in org.orekit.propagation.events.handlers

Enumerate for actions to be performed when an event occurs.

eventIsEnabled(SpacecraftState, S, double) - Method in interface org.orekit.propagation.events.EnablingPredicate

Compute an event enabling function of state.

eventOccurred(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Handle the event.

eventOccurred(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.events.FieldEventDetector

Handle the event.

eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldContinueOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler

eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.

eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnDecreasing

Handle a detection event and choose what to do next.

eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnIncreasing

Handle a detection event and choose what to do next.

eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AbstractDetector

Handle the event.

eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AdapterDetector

Handle the event.

eventOccurred(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.EventDetector

Handle the event.

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(SpacecraftState, T, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler

eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing

Handle a detection event and choose what to do next.

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing

Handle a detection event and choose what to do next.

EventShifter<T extends EventDetector> - Class in org.orekit.propagation.events

Wrapper shifting events occurrences times.

EventShifter(T, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter

Build a new instance.

EventsLogger - Class in org.orekit.propagation.events

This class logs events detectors events during propagation.

EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger

Simple constructor.

EventsLogger.LoggedEvent - Class in org.orekit.propagation.events

Class for logged events entries.

EventSlopeFilter<T extends EventDetector> - Class in org.orekit.propagation.events

Wrapper used to detect only increasing or decreasing events.

EventSlopeFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter

Wrap an event detector.

EventState<T extends EventDetector> - Class in org.orekit.propagation.events

This class handles the state for one event detector during integration steps.

EventState(T) - Constructor for class org.orekit.propagation.events.EventState

Simple constructor.

EventState.EventOccurrence - Class in org.orekit.propagation.events

Class to hold the data related to an event occurrence that is needed to decide how to modify integration.

EXT - org.orekit.files.sp3.SP3File.SP3OrbitType

extrapolated or predicted.

ExtendedPVCoordinatesProvider - Interface in org.orekit.utils

Interface for PV coordinates providers that also support fields.

extendListOfLists(List<List<Double>>, int, int, double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Extend a list of lists of coefficients if needed.

extractRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Extract a range of the map.

F

f - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Equinoctial frame f vector.

F0 - Static variable in enum org.orekit.gnss.Frequency

Common frequency F0 in MHz (10.23 MHz).

Facet(Vector3D, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet

Simple constructor.

FactoryManagedFrame - Class in org.orekit.frames

Base class for the predefined frames that are managed by FramesFactory.

FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame

Simple constructor.

FEASIBLE_MEASUREMENT_WHEN_NEGATIVE - org.orekit.estimation.measurements.generation.SignSemantic

Semantic for detectors that have negative g function when measurements are feasible.

FEASIBLE_MEASUREMENT_WHEN_POSITIVE - org.orekit.estimation.measurements.generation.SignSemantic

Semantic for detectors that have positive g function when measurements are feasible.

FEBRUARY - org.orekit.time.Month

February.

feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager

Feed a data file loader by browsing all data providers.

feed(Pattern, DataLoader) - Method in class org.orekit.data.ClasspathCrawler

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader) - Method in interface org.orekit.data.DataProvider

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader) - Method in class org.orekit.data.DirectoryCrawler

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader) - Method in class org.orekit.data.NetworkCrawler

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader) - Method in class org.orekit.data.ZipJarCrawler

Feed a data file loader by browsing the data collection.

FES_CHAT_EPSILON_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES C hat and epsilon tides files.

FES_CNM_SNM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES Cnm, Snm tides files.

FES_HF_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES Hf tides files.

FESCHatEpsilonReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides files following the fes2004.dat format.

FESCHatEpsilonReader(String, double, double, OceanLoadDeformationCoefficients, Map<Integer, Double>) - Constructor for class org.orekit.forces.gravity.potential.FESCHatEpsilonReader

Simple constructor.

FESCnmSnmReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides files following the fes2004_Cnm-Snm.dat format.

FESCnmSnmReader(String, double) - Constructor for class org.orekit.forces.gravity.potential.FESCnmSnmReader

Simple constructor.

FieldAbsoluteDate<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.time

This class represents a specific instant in time.

FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate

Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).

FieldAbsoluteDate(Field<T>, int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, int, int, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, int, Month, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, String, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location (parsed from a string) in a time scale.

FieldAbsoluteDate(Field<T>, Date, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an AbsoluteDate.

FieldAbsoluteDate(Field<T>, DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an elapsed duration since to another instant.

FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an elapsed duration since to another instant.

FieldAbsoluteDate(FieldAbsoluteDate<T>, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.

FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an elapsed duration since to another instant.

FieldAbstractAnalyticalPropagator<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.analytical

Common handling of FieldPropagator methods for analytical propagators.

FieldAbstractAnalyticalPropagator(Field<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Build a new instance.

FieldAbstractDetector<D extends FieldEventDetector<T>,T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Common parts shared by several orbital events finders.

FieldAbstractDetector(T, T, int, FieldEventHandler<? super D, T>) - Constructor for class org.orekit.propagation.events.FieldAbstractDetector

Build a new instance.

FieldAbstractIntegratedPropagator<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.integration

Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.

FieldAbstractIntegratedPropagator(Field<T>, FieldODEIntegrator<T>, boolean) - Constructor for class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Build a new instance.

FieldAbstractIntegratedPropagator.MainStateEquations<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.integration

Differential equations for the main state (orbit, attitude and mass).

FieldAbstractPropagator<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation

Common handling of Propagator methods for analytical propagators.

FieldAbstractPropagator(Field<T>) - Constructor for class org.orekit.propagation.FieldAbstractPropagator

Build a new instance.

FieldAdditionalEquations<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.integration

This interface allows users to add their own differential equations to a numerical propagator.

FieldAdditionalStateProvider<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation

This interface represents providers for additional state data beyond SpacecraftState.

FieldAltitudeDetector<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Finder for satellite altitude crossing events.

FieldAltitudeDetector(T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector

Build a new altitude detector.

FieldAltitudeDetector(T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector

Build a new altitude detector.

FieldAltitudeDetector(T, T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector

Build a new altitude detector.

FieldAngularCoordinates<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.utils

Simple container for rotation / rotation rate pairs, using RealFieldElement.

FieldAngularCoordinates(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.

FieldAngularCoordinates(FieldRotation<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a FieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.

FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a rotation/rotation rate pair.

FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a rotation / rotation rate / rotation acceleration triplet.

FieldAngularCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another one.

FieldApsideDetector<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Finder for apside crossing events.

FieldApsideDetector(FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector

Build a new instance.

FieldApsideDetector(T, FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector

Build a new instance.

FieldAttitude<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.attitudes

This class handles attitude definition at a given date.

FieldAttitude(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude

Builds an instance for a regular Attitude.

FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude

Creates a new instance.

FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldAttitude

Creates a new instance.

FieldAttitude(FieldAbsoluteDate<T>, Frame, Rotation, Vector3D, Vector3D, Field<T>) - Constructor for class org.orekit.attitudes.FieldAttitude

Creates a new instance.

FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude

Creates a new instance.

FieldBodiesElements<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.data

Elements of the bodies having an effect on nutation.

FieldBodiesElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements

Simple constructor.

FieldBoundedPropagator<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation

This interface is intended for ephemerides valid only during a time range.

FieldCartesianOrbit<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits

This class holds Cartesian orbital parameters.

FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit

Constructor from any kind of orbital parameters.

FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCartesianOrbit

Constructor from Cartesian parameters.

FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldCartesianOrbit

Constructor from Cartesian parameters.

FieldCircularOrbit<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits

This class handles circular orbital parameters.

FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Constructor from any kind of orbital parameters.

FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Constructor from Cartesian parameters.

FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Constructor from Cartesian parameters.

FieldCircularOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Creates a new instance.

FieldCircularOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Creates a new instance.

FieldContinueOnEvent<KK extends FieldEventDetector<T>,T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Event handler which will always return continue as a state.

FieldContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldContinueOnEvent

FieldDateDetector<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Finder for date events.

FieldDateDetector(FieldAbsoluteDate<T>) - Constructor for class org.orekit.propagation.events.FieldDateDetector

Build a new instance.

FieldDateDetector(T, T, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector

Build a new instance.

FieldDelaunayArguments<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.data

Delaunay arguments used for nutation or tides.

FieldDelaunayArguments(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments

Simple constructor.

FieldEcksteinHechlerPropagator<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.analytical

This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider, mass and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider, mass and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Private helper constructor.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, mass and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, mass and potential provider.

FieldEclipseDetector<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Finder for satellite eclipse related events.

FieldEclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double, Field<T>) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector

Build a new eclipse detector.

FieldEclipseDetector(T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector

Build a new eclipse detector.

FieldEclipseDetector(T, T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector

Build a new eclipse detector.

FieldElevationDetector<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.

FieldElevationDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.

FieldElevationDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.

FieldEquinoctialOrbit<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits

This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.

FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Constructor from any kind of orbital parameters.

FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Constructor from Cartesian parameters.

FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Constructor from Cartesian parameters.

FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Creates a new instance.

FieldEquinoctialOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Creates a new instance.

FieldEventDetector<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.events

This interface represents space-dynamics aware events detectors.

FieldEventHandler<KK extends FieldEventDetector<T>,T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.events.handlers

An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.

FieldEventHandler.Action - Enum in org.orekit.propagation.events.handlers

Enumerate for actions to be performed when an event occurs.

FieldEventsLogger<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

This class logs events detectors events during propagation.

FieldEventsLogger() - Constructor for class org.orekit.propagation.events.FieldEventsLogger

Simple constructor.

FieldEventsLogger.FieldLoggedEvent<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Class for logged events entries.

FieldEventState<D extends FieldEventDetector<T>,T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

This class handles the state for one event detector during integration steps.

FieldEventState(D) - Constructor for class org.orekit.propagation.events.FieldEventState

Simple constructor.

FieldEventState.EventOccurrence<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Class to hold the data related to an event occurrence that is needed to decide how to modify integration.

FieldGeodeticPoint<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.bodies

Point location relative to a 2D body surface, using RealFieldElement.

FieldGeodeticPoint(T, T, T) - Constructor for class org.orekit.bodies.FieldGeodeticPoint

Build a new instance.

FieldIntegratedEphemeris<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.integration

This class stores sequentially generated orbital parameters for later retrieval.

FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, boolean, FieldDenseOutputModel<T>, Map<String, T[]>, List<FieldAdditionalStateProvider<T>>, String[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris

Creates a new instance of IntegratedEphemeris.

FieldKeplerianOrbit<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits

This class handles traditional Keplerian orbital parameters.

FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Constructor from any kind of orbital parameters.

FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Constructor from Cartesian parameters.

FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Constructor from Cartesian parameters.

FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Creates a new instance.

FieldKeplerianOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Creates a new instance.

FieldKeplerianPropagator<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.analytical

Simple Keplerian orbit propagator.

FieldKeplerianPropagator(FieldOrbit<T>) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build a propagator from orbit only.

FieldKeplerianPropagator(FieldOrbit<T>, double) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build a propagator from orbit and central attraction coefficient μ.

FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build a propagator from orbit and attitude provider.

FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build a propagator from orbit, attitude provider and central attraction coefficient μ.

FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, double, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

FieldModeHandler<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.integration

Common interface for all propagator mode handlers initialization.

FieldNodeDetector<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events

Finder for node crossing events.

FieldNodeDetector(FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector

Build a new instance.

FieldNodeDetector(T, FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector

Build a new instance.

FieldNumericalPropagator<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.numerical

This class propagates orbits using numerical integration.

FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator

Create a new instance of NumericalPropagator, based on orbit definition mu.

FieldOfView - Class in org.orekit.propagation.events

Class representing a spacecraft sensor Field Of View.

FieldOfView(Vector3D, Vector3D, double, int, double) - Constructor for class org.orekit.propagation.events.FieldOfView

Build Field Of View with a regular polygon shape.

FieldOfView(Vector3D, Vector3D, double, Vector3D, double, double) - Constructor for class org.orekit.propagation.events.FieldOfView

Build a Field Of View with dihedral shape (i.e.

FieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FieldOfView

Build a new instance.

FieldOfViewDetector - Class in org.orekit.propagation.events

Finder for target entry/exit events with respect to a satellite sensor Field Of View.

FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector

Build a new instance.

FieldOrbit<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits

This class handles orbital parameters.

FieldOrbit(Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldOrbit

Default constructor.

FieldOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldOrbit

Set the orbit from Cartesian parameters.

FieldOrekitFixedStepHandler<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware fixed size step handler.

FieldOrekitStepHandler<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step handler.

FieldOrekitStepHandlerMultiplexer<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.sampling

This class gathers several OrekitStepHandler instances into one.

FieldOrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer

Simple constructor.

FieldOrekitStepInterpolator<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step interpolator.

FieldOrekitStepNormalizer<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.sampling

This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.

FieldOrekitStepNormalizer(T, FieldOrekitFixedStepHandler<T>) - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Simple constructor.

FieldPoleCorrection<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.frames

Simple container class for pole correction parameters.

FieldPoleCorrection(T, T) - Constructor for class org.orekit.frames.FieldPoleCorrection

Simple constructor.

FieldPropagator<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation

This interface provides a way to propagate an orbit at any time.

FieldPVCoordinates<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.utils

Simple container for Position/Velocity pairs, using RealFieldElement.

FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor.

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a FieldPVCoordinates from a field and a regular PVCoordinates.

FieldPVCoordinates(FieldVector3D<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a FieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.

FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a FieldPVCoordinates triplet with zero acceleration.

FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a FieldPVCoordinates triplet.

FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Subtractive constructor.

FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor.

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor.

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinatesProvider<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.utils

Interface for PV coordinates providers.

FieldSpacecraftState<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation

This class is the representation of a complete state holding orbit, attitude and mass information at a given date.

FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Convert a SpacecraftState.

FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit only.

FieldSpacecraftState(FieldOrbit<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit only.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit and attitude provider.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit and attitude provider.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit, attitude provider and mass.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit, attitude provider and mass.

FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Create a new instance from orbit and mass.

FieldSpacecraftState(FieldOrbit<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Create a new instance from orbit and mass.

FieldStateMapper<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.integration

This class maps between raw double elements and FieldSpacecraftState instances.

FieldStateMapper(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper

Simple constructor.

FieldStopOnDecreasing<KK extends FieldEventDetector<T>,T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

FieldStopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnDecreasing

FieldStopOnEvent<KK extends FieldEventDetector<T>,T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Event handler which will always return continue as a state.

FieldStopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnEvent

FieldStopOnIncreasing<KK extends FieldEventDetector<T>,T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

FieldStopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnIncreasing

FieldTimeDerivativesEquations<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.numerical

Interface summing up the contribution of several forces into orbit and mass derivatives.

FieldTimeInterpolable<T extends FieldTimeInterpolable<T,KK>,KK extends org.hipparchus.RealFieldElement<KK>> - Interface in org.orekit.time

This interface represents objects that can be interpolated in time.

FieldTimeShiftable<T extends FieldTimeInterpolable<T,KK>,KK extends org.hipparchus.RealFieldElement<KK>> - Interface in org.orekit.time

This interface represents objects that can be shifted in time.

FieldTimeSpanMap<T,D extends org.hipparchus.RealFieldElement<D>> - Class in org.orekit.utils

Container for objects that apply to spans of time.

FieldTimeSpanMap(T, Field<D>) - Constructor for class org.orekit.utils.FieldTimeSpanMap

Create a map containing a single object, initially valid throughout the timeline.

FieldTimeSpanMap.Transition<S,D extends org.hipparchus.RealFieldElement<D>> - Class in org.orekit.utils

Local class holding transition times.

FieldTimeStamped<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.time

This interface represents objects that have a AbsoluteDate date attached to them.

FieldTransform<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.frames

Transformation class in three dimensional space.

FieldTransform(Field<T>, Transform) - Constructor for class org.orekit.frames.FieldTransform

Build a transform from a regular transform.

FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a rotation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a rotation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a rotation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a translation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a translation transform, with its first time derivative.

FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a translation transform, with its first and second time derivatives.

FieldTransform(FieldAbsoluteDate<T>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a transform by combining two existing ones.

FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a rotation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a translation transform, with its first time derivative.

FieldTransformGenerator<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.frames

Generator to use field transforms in GenericTimeStampedCache.

FieldTransformGenerator(Field<T>, int, TransformProvider, double) - Constructor for class org.orekit.frames.FieldTransformGenerator

simple constructor.

FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.

FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for 1950 dates: 1950-01-01.

fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a single vector.

fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a single vector.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EOPHistoryLoader

Load celestial body.

filter(boolean) - Method in class org.orekit.utils.ParameterDriversList

Filter parameters to keep only one type of selection status.

filter(NamedData) - Method in interface org.orekit.data.DataFilter

Filter the named data.

filter(NamedData) - Method in class org.orekit.data.GzipFilter

Filter the named data.

filter(NamedData) - Method in class org.orekit.data.UnixCompressFilter

Filter the named data.

FilterType - Enum in org.orekit.propagation.events

Enumerate for filtering events.

finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.Model

Finalize estimation.

findByName(String) - Method in class org.orekit.utils.ParameterDriversList

Find a delegating driver by name.

findEOP(Frame) - Static method in class org.orekit.frames.FramesFactory

Retrieve EOP from a frame hierarchy.

findSatelliteAntenna(SatelliteSystem, int) - Method in class org.orekit.gnss.antenna.AntexLoader

Find the time map for a specific satellite antenna.

FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion

Propagator converter using finite differences to compute the Jacobian.

FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter

Simple constructor.

fit() - Method in class org.orekit.utils.SecularAndHarmonic

Fit parameters.

FIT - org.orekit.files.sp3.SP3File.SP3OrbitType

fitted.

FixedNumberInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.

FixedNumberInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid

Constructor.

FixedRate - Class in org.orekit.attitudes

This class handles a simple attitude provider at constant rate around a fixed axis.

FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate

Creates a new instance.

FixedStepSelector - Class in org.orekit.time

Selector generating a continuous stream of dates separated by a constant step.

FixedStepSelector(double, TimeScale) - Constructor for class org.orekit.time.FixedStepSelector

Simple constructor.

FixedTransformProvider - Class in org.orekit.frames

Transform provider using fixed transform.

FixedTransformProvider(Transform) - Constructor for class org.orekit.frames.FixedTransformProvider

Simple constructor.

FixedTroposphericDelay - Class in org.orekit.models.earth

A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.

FixedTroposphericDelay(double[], double[], double[][]) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay

Creates a new FixedTroposphericDelay instance.

FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay

Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the DataProvidersManager.

FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Parameter name for flow rate.

FootprintOverlapDetector - Class in org.orekit.propagation.events

Detector triggered by geographical region entering/leaving a spacecraft sensor Field Of View.

FootprintOverlapDetector(FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector

Build a new instance.

ForceModel - Interface in org.orekit.forces

This interface represents a force modifying spacecraft motion.

Frame - Class in org.orekit.frames

Tridimensional references frames class.

Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame

Build a non-inertial frame from its transform with respect to its parent.

Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame

Build a frame from its transform with respect to its parent.

Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame

Build a non-inertial frame from its transform with respect to its parent.

Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame

Build a frame from its transform with respect to its parent.

FRAME_ALREADY_ATTACHED - org.orekit.errors.OrekitMessages

FRAME_ANCESTOR_OF_BOTH_FRAMES - org.orekit.errors.OrekitMessages

FRAME_ANCESTOR_OF_NEITHER_FRAME - org.orekit.errors.OrekitMessages

FRAME_NO_NTH_ANCESTOR - org.orekit.errors.OrekitMessages

FRAME_NOT_ATTACHED - org.orekit.errors.OrekitMessages

FrameAncestorException - Exception in org.orekit.errors

This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.

FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException

Simple constructor.

FRAMES_MISMATCH - org.orekit.errors.OrekitMessages

FramesFactory - Class in org.orekit.frames

Factory for predefined reference frames.

freeze() - Method in class org.orekit.frames.FieldTransform

Get a frozen transform.

freeze() - Method in class org.orekit.frames.Transform

Get a frozen transform.

FREQ_OFFSET - org.orekit.files.ccsds.Keyword

Meta-data: Frequency offset.

Frequency - Enum in org.orekit.gnss

Enumerate for GNSS frequencies.

FrequencyPattern - Class in org.orekit.gnss.antenna

Pattern for GNSS antenna model on one frequency.

FrequencyPattern(Vector3D, PhaseCenterVariationFunction) - Constructor for class org.orekit.gnss.antenna.FrequencyPattern

Simple constructor.

FunctionalDetector - Class in org.orekit.propagation.events

A detector that implements the FunctionalDetector.g(SpacecraftState) function using a lambda that can be set using FunctionalDetector.withFunction(ToDoubleFunction).

FunctionalDetector() - Constructor for class org.orekit.propagation.events.FunctionalDetector

Create an event detector with the default values.

FunctionalDetector.GFunction - Interface in org.orekit.propagation.events

Deprecated.

Use ToDoubleFunction instead. Will be removed in next major release.

FundamentalNutationArguments - Class in org.orekit.data

Class computing the fundamental arguments for nutation and tides.

FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String) - Constructor for class org.orekit.data.FundamentalNutationArguments

Build a model of fundamental arguments from an IERS table file.

FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments

Build a model of fundamental arguments from an IERS table file.

FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate

Dummy date at infinity in the future direction.

G

g - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Equinoctial frame g vector.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector

g(SpacecraftState) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.FunctionalDetector

g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundAtNightDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector

g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector

Compute the value of the detection function.

G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants

Standard gravity constant, used in maneuvers definition: 9.80665 m/s².

G01 - org.orekit.gnss.Frequency

GPS L1 (1575.42 MHz).

G02 - org.orekit.gnss.Frequency

GPS L2 (1227.6 MHz).

G05 - org.orekit.gnss.Frequency

GPS L5 (1176.45 MHz).

GAL - org.orekit.files.sp3.SP3File.TimeSystem

GALILEO.

Galileo - Class in org.orekit.gnss.attitude

Attitude providers for Galileo navigation satellites.

Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo

Simple constructor.

GALILEO - org.orekit.files.sp3.SP3File.SP3FileType

Galileo only file.

GALILEO - org.orekit.gnss.SatelliteSystem

Galileo system.

GALILEO_0A - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

Galileo In-Orbit Validation Element A (GIOVE-A).

GALILEO_0A - org.orekit.gnss.antenna.SatelliteType

Galileo In-Orbit Validation Element A (GIOVE-A).

GALILEO_0B - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

Galileo In-Orbit Validation Element B (GIOVE-B).

GALILEO_0B - org.orekit.gnss.antenna.SatelliteType

Galileo In-Orbit Validation Element B (GIOVE-B).

GALILEO_1 - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

Galileo IOV : GSAT 0101-0104.

GALILEO_1 - org.orekit.gnss.antenna.SatelliteType

Galileo IOV : GSAT 0101-0104.

GALILEO_2 - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

Galileo FOC : GSAT 0201-0222.

GALILEO_2 - org.orekit.gnss.antenna.SatelliteType

Galileo FOC : GSAT 0201-0222.

GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.

GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for Galileo System Time: 1999-08-22.

GalileoScale - Class in org.orekit.time

Galileo system time scale.

GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the Γ^m_n,s(γ) function from equation 2.7.1-(13).

GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Simple constructor.

GCRF - org.orekit.files.ccsds.CCSDSFrame

Geocentric Celestial Reference Frame.

GCRF - org.orekit.frames.Predefined

GCRF frame.

GEGOUT - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Coefficients computed by Pascal Gégout, CNRS / UMR5563 (GET).

generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.ContinuousScheduler

Generate a sequence of measurements.

generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.EventBasedScheduler

Generate a sequence of measurements.

generate(List<OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler

Generate a sequence of measurements.

generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator

Generate measurements.

generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator

Generate a chronologically sorted list of entries to be cached.

generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator

Generate a chronologically sorted list of entries to be cached.

generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator

Generate a chronologically sorted list of entries to be cached.

generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OMMFile

Generate a CartesianOrbit from the KeplerianOrbit.

generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OPMFile

Generate a CartesianOrbit from the OPM state vector data.

generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OMMFile

Generate a KeplerianOrbit based on the OMM mean Keplerian elements.

generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OPMFile

Generate a KeplerianOrbit from the OPM Keplerian elements if hasKeplerianElements is true, or from the state vector data otherwise.

generateSpacecraftState() - Method in class org.orekit.files.ccsds.OMMFile

Generate spacecraft state from the KeplerianOrbit generated by generateKeplerianOrbit.

generateSpacecraftState() - Method in class org.orekit.files.ccsds.OPMFile

Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.

generateTLE() - Method in class org.orekit.files.ccsds.OMMFile

Generate TLE from OMM file.

Generator - Class in org.orekit.estimation.measurements.generation

Main generator for observed measurements.

Generator() - Constructor for class org.orekit.estimation.measurements.generation.Generator

Build a generator with no sequences generator.

GenericGNSS - Class in org.orekit.gnss.attitude

Attitude providers for navigation satellites for which no specialized model is known.

GenericGNSS(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GenericGNSS

Simple constructor.

GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils

Generic thread-safe cache for time-stamped data.

GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache

Simple constructor.

GeodeticPoint - Class in org.orekit.bodies

Point location relative to a 2D body surface.

GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint

Build a new instance.

GeographicZoneDetector - Class in org.orekit.propagation.events

Detector for entry/exit of a zone defined by geographic boundaries.

GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector

Build a detector.

GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector

Build a new detector.

Geoid - Class in org.orekit.models.earth

A geoid is a level surface of the gravity potential of a body.

Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid

Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.

GeoMagneticElements - Class in org.orekit.models.earth

Contains the elements to represent a magnetic field at a single point.

GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements

Construct a new element with the given field vector.

GeoMagneticField - Class in org.orekit.models.earth

Used to calculate the geomagnetic field at a given geodetic point on earth.

GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField

Create a new geomagnetic field model with the given parameters.

GeoMagneticFieldFactory - Class in org.orekit.models.earth

Factory for different GeoMagneticField models.

GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth

The currently supported geomagnetic field models.

GeoMagneticModelLoader - Class in org.orekit.models.earth

Loads geomagnetic field models from a given input stream.

GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader

get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Get the entry valid at a specified date.

get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap

Get the entry valid at a specified date.

get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

The Kp index is derived from the Ap index.

get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters

Get the last 24H mean geomagnetic index.

getA() - Method in class org.orekit.bodies.Ellipse

Get the semi major axis.

getA() - Method in class org.orekit.bodies.Ellipsoid

Get the length of the first semi-axis.

getA() - Method in class org.orekit.files.ccsds.OGMFile

Get the orbit semi-major axis.

getA() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model

Returns the a coefficients array.

getA() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader

Returns the a coefficients array.

getA() - Method in class org.orekit.orbits.CartesianOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.CircularOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.KeplerianOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.Orbit

Get the semi-major axis.

getA() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the semi-major axis.

getA() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get A = sqrt(μ * a).

getA() - Method in class org.orekit.propagation.SpacecraftState

Get the semi-major axis.

getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader

Returns a copy of the abscissa grid for the interpolation function.

getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition

Get the transition field absolute date.

getAcceleration() - Method in class org.orekit.frames.FieldTransform

Get the second time derivative of the translation.

getAcceleration() - Method in class org.orekit.frames.Transform

Get the second time derivative of the translation.

getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates

Gets the acceleration.

getAcceleration() - Method in class org.orekit.utils.PVCoordinates

Gets the acceleration.

getAccuracy() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

Get the formal accuracy for this satellite.

getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence

Get the user requested action.

getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence

Get the user requested action.

getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the adapted propagator.

getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState

Get an additional state.

getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState

Get an additional state.

getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider

Get the additional state.

getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider

Get the additional state.

getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider

Get the additional state.

getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper

Compute the length of the one-dimensional additional state array needed.

getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator

Get an unmodifiable list of providers for additional state.

getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get an unmodifiable list of providers for additional state.

getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator

Get an unmodifiable list of providers for additional state.

getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator

Get an unmodifiable list of providers for additional state.

getAdditionalStates() - Method in class org.orekit.propagation.FieldSpacecraftState

Get an unmodifiable map of additional states.

getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState

Get an unmodifiable map of additional states.

getADot() - Method in class org.orekit.orbits.CartesianOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.CircularOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.Orbit

Get the semi-major axis derivative.

getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the value of the central body reference radius.

getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the central body reference radius.

getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the value of the central body reference radius.

getAf0() - Method in class org.orekit.gnss.GPSAlmanac

getAf0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Zeroth Order Clock Correction.

getAf1() - Method in class org.orekit.gnss.GPSAlmanac

getAf1() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the First Order Clock Correction.

getAf2() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Second Order Clock Correction.

getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition

Get the entry valid after transition.

getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the entry valid after transition.

getAgency() - Method in class org.orekit.files.sp3.SP3File

Returns the agency that prepared this SP3 file.

getAgencyName() - Method in class org.orekit.gnss.RinexHeader

Get name of the agency.

getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector

Get the alignment angle (rad).

getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache

Get all of the data in this cache.

getAllForceModels() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Get the list of all force models.

getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get all the force models, perturbing forces and Newtonian attraction included.

getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get all the force models, perturbing forces and Newtonian attraction included.

getAlmanacs() - Method in class org.orekit.gnss.SEMParser

Gets all the GPS almanacs read from the file.

getAlmanacs() - Method in class org.orekit.gnss.YUMAParser

Gets all the GPS almanacs read from the file.

getAlpha() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Returns the alpha coefficients array.

getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get direction cosine α for central body.

getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit

Get the latitude argument.

getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit

Get the latitude argument.

getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit

Get the latitude argument derivative.

getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit

Get the latitude argument derivative.

getAlphaE() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric latitude argument.

getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentric latitude argument.

getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric latitude argument derivative.

getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentric latitude argument derivative.

getAlphaM() - Method in class org.orekit.orbits.CircularOrbit

Get the mean latitude argument.

getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the mean latitude argument.

getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit

Get the mean latitude argument derivative.

getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the mean latitude argument derivative.

getAlphaV() - Method in class org.orekit.orbits.CircularOrbit

Get the true latitude argument.

getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the true latitude argument.

getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit

Get the true latitude argument derivative.

getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the true latitude argument derivative.

getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the altitude.

getAltitude() - Method in class org.orekit.bodies.GeodeticPoint

Get the altitude.

getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector

Get the threshold altitude value.

getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector

Get the threshold altitude value.

getAncestor(int) - Method in class org.orekit.frames.Frame

Get the n^th ancestor of the frame.

getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector

Get the fixed angle to be crossed (radians).

getAngleType() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for angleType.

getAngular() - Method in class org.orekit.frames.FieldTransform

Get the underlying elementary angular part.

getAngular() - Method in class org.orekit.frames.Transform

Get the underlying elementary angular part.

getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates

Get the angular velocity (spin) of this point as seen from the origin.

getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates

Get the angular velocity (spin) of this point as seen from the origin.

getAnomaly() - Method in class org.orekit.files.ccsds.OGMFile

Get the orbit anomaly.

getAnomaly(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the anomaly.

getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit

Get the anomaly.

getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the anomaly derivative.

getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit

Get the anomaly derivative.

getAnomalyType() - Method in class org.orekit.files.ccsds.OGMFile

Get the type of anomaly (true or mean).

getAntennaAzimuth() - Method in class org.orekit.gnss.RinexHeader

Get the azimuth of the zero direction of a fixed antenna.

getAntennaBSight() - Method in class org.orekit.gnss.RinexHeader

Get the antenna B.Sight.

getAntennaHeight() - Method in class org.orekit.gnss.RinexHeader

Get the antenna height.

getAntennaNumber() - Method in class org.orekit.gnss.RinexHeader

Get the number of the antenna.

getAntennaPhaseCenter() - Method in class org.orekit.gnss.RinexHeader

Get the antenna phasecenter.

getAntennaReferencePoint() - Method in class org.orekit.gnss.RinexHeader

Get the position of antenna reference point for antenna on vehicle.

getAntennaType() - Method in class org.orekit.gnss.RinexHeader

Get the type of the antenna.

getAntennaZeroDirection() - Method in class org.orekit.gnss.RinexHeader

Get the zero direction of antenna.

getAp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the A_p geomagnetic indices.

getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters

Get the A_p geomagnetic indices.

getApproxPos() - Method in class org.orekit.gnss.RinexHeader

Get the Approximate Marker Position.

getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet

Get facet area.

getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Get astronomical amplitudes map.

getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get the atmospheric model.

getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the attitude.

getAttitude() - Method in class org.orekit.propagation.SpacecraftState

Get the attitude.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the attitude override used for the maneuver.

getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the Attitude Provider to use during maneuver.

getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator

Get attitude provider.

getAttitudeProvider() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Get the attitudeProvider.

getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get attitude provider.

getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator

Get attitude provider.

getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get the attitude provider.

getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper

Get the attitude provider.

getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator

Get attitude provider.

getAvailableDerivatives() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get which derivatives of position are available in this ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Get the available satellite numbers.

getAverageFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the 81 day average of F10.7 solar flux centered on current day.

getAverageFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters

Get the value of the 81 day average of F10.7 solar flux centered on current day.

getAzimuth(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the azimuth of a point with regards to the topocentric frame center point.

getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the azimuth of a point with regards to the topocentric frame center point.

getB() - Method in class org.orekit.bodies.Ellipse

Get the semi minor axis.

getB() - Method in class org.orekit.bodies.Ellipsoid

Get the length of the second semi-axis.

getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get B = sqrt(1 - e²).

getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation

Get the base frame associated with the station.

getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the base system state at given date, without compensation.

getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the base system state at given date, without compensation.

getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the base system state at given date, without compensation.

getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the base system state at given date, without compensation.

getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the base weight associated with the measurement

getBaseWeight() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the base weight associated with the measurement

getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the base weight associated with the measurement

getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get state vector dimension without additional parameters.

getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get state vector dimension without additional parameters.

getBDT() - Static method in class org.orekit.time.TimeScalesFactory

Get the BeiDou Navigation Satellite System time scale.

getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector

Get the beacon at the center of the proximity zone.

getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition

Get the entry valid before transition.

getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the entry valid before transition.

getBeta() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Returns the beta coefficients array.

getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get direction cosine β for central body.

getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Get third body.

getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Get a celestial body.

getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing

Get the body frame.

getBodyFrame() - Method in interface org.orekit.bodies.BodyShape

Get body frame related to body shape.

getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get body frame related to body shape.

getBodyFrame() - Method in class org.orekit.models.earth.Geoid

getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody

Get a body oriented, body centered frame.

getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector

Get the body shape.

getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector

Get the body shape.

getBStar() - Method in class org.orekit.files.ccsds.OMMFile

Get the SGP/SGP4 drag-like coefficient.

getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the ballistic coefficient.

getBuilder() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler

Get the measurements builder.

getC() - Method in class org.orekit.bodies.Ellipsoid

Get the length of the third semi-axis.

getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get C = 1 + p² + q².

getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid

Get the fully normalized coefficient C_2n,0 for the normal gravity potential.

getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration

Get the number of slots to use in caches.

getCalendarWeek() - Method in class org.orekit.time.DateComponents

Get the calendar week number.

getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the number of calls to the differential equations computation method.

getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the number of calls to the differential equations computation method.

getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month

Get the capitalized three letters abbreviation.

getCapitalizedName() - Method in enum org.orekit.time.Month

Get the capitalized full name.

getCartesian() - Method in class org.orekit.frames.FieldTransform

Get the underlying elementary Cartesian part.

getCartesian() - Method in class org.orekit.frames.Transform

Get the underlying elementary Cartesian part.

getCartesianIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the intersection point of a line with the surface of the body.

getCartesianIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the intersection point of a line with the surface of the body.

getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).

getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName

Get the celestial body corresponding to the CCSDS constant.

getCenter() - Method in class org.orekit.bodies.Ellipse

Get the center of the 2D ellipse.

getCenter() - Method in class org.orekit.models.earth.tessellation.Tile

Get the center point.

getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector

Get the direction of FOV center.

getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the CelestialBody corresponding to the center name.

getCenterMass() - Method in class org.orekit.gnss.RinexHeader

Get the current center of mass of vehicle in body fixed coordinate system.

getCenterName() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame

Get the CCSDS center name.

getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the origin of reference frame.

getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse

Find the center of curvature (point on the evolute) at the nadir of a point.

getCentralBody() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Get the central body.

getChildren() - Method in class org.orekit.frames.OrphanFrame

Get all children of the instance.

getCic() - Method in class org.orekit.gnss.GPSAlmanac

getCic() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.

getCircularEx() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the circular eccentricity vector.

getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the circular eccentricity vector.

getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the circular eccentricity vector derivative.

getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the circular eccentricity vector derivative.

getCircularEy() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the circular eccentricity vector.

getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the circular eccentricity vector.

getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the circular eccentricity vector derivative.

getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the circular eccentricity vector derivative.

getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the CIRF2000 reference frame.

getCis() - Method in class org.orekit.gnss.GPSAlmanac

getCis() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.

getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the C_j coefficient.

getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the classification.

getClassificationType() - Method in class org.orekit.files.ccsds.OMMFile

Get the classification type.

getClkOffset() - Method in class org.orekit.gnss.RinexHeader

Get the realtime-derived receiver clock offset.

getClockCorrection() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate

Returns the clock correction value.

getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station clock (which is related to measurement date).

getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite

Get the clock offset parameter driver.

getClockRateChange() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate

Returns the clock rate.

getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Get the closest TLE to the selected date.

getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Get the load deformation coefficients for ocean tides.

getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

Get the coefficients for a given site.

getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms

Computes the coefficients involved in the contributions.

getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms

Get the prefix for short period coefficients keys.

getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils

Combine two transform providers.

getComment() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the meta-data comment.

getComment() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get the maneuvers data comment, each string in the list corresponds to one line of comment.

getComment() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Get the meta-data comment.

getComponents(int) - Method in class org.orekit.time.AbsoluteDate

Split the instance into date/time components for a local time.

getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate

Split the instance into date/time components for a local time.

getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate

Split the instance into date/time components for a time zone.

getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate

Split the instance into date/time components for a time zone.

getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Split the instance into date/time components.

getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Split the instance into date/time components.

getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the constant gravity field coefficients provider from the first supported file.

getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get a time-independent provider for read spherical harmonics coefficients.

getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the constant gravity field coefficients provider from the first supported file.

getConventions() - Method in class org.orekit.files.ccsds.ODMFile

Get IERS conventions.

getConventions() - Method in class org.orekit.files.ccsds.ODMParser

Get IERS conventions.

getConventions() - Method in class org.orekit.files.ccsds.TDMParser

Get IERS conventions.

getConventions() - Method in class org.orekit.frames.EOPHistory

Get the IERS conventions to which these EOP apply.

getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion

Find a converter between specified ITRF frames.

getCoordinates() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the coordinates for this ephemeris segment.

getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getCoordinates() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getCoordinates(SpacecraftState, int, DSFactory) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement

Get Cartesian coordinates as derivatives.

getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File

Returns the coordinate system of the entries in this orbit file.

getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the estimated measurement.

getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.Model

Get the estimated measurement.

getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the corrected spacecraft states.

getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.Model

Get the corrected spacecraft states.

getCorrection() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection

Get the Phase Shift Corrections.

getCorrection() - Method in class org.orekit.gnss.RinexLoader.Parser.ScaleFactorCorrection

Get the Scale Factor.

getCorrectionAngle1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the correctionAngle1.

getCorrectionAngle2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the correctionAngle2.

getCorrectionDoppler() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the correctionDoppler.

getCorrectionRange() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the correctionRange.

getCorrectionReceive() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the correctionReceive.

getCorrectionsApplied() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the correctionApplied.

getCorrectionTransmit() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the correctionTransmit.

getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.Position

Get the correlation coefficients matrix.

getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.PV

Get the correlation coefficients matrix.

getCosparID() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get COSPAR ID.

getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the evaluations counter.

getCovariance() - Method in class org.orekit.estimation.sequential.MeasurementDecorator

getCovarianceComment() - Method in class org.orekit.files.ccsds.OGMFile

Get the comment for covariance.

getCovarianceMatrices() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get the list of Covariance Matrices.

getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.Position

Get the covariance matrix.

getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.PV

Get the covariance matrix.

getCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile

Get the Position/Velocity covariance matrix.

getCovRefFrame() - Method in class org.orekit.files.ccsds.OGMFile

Get coordinate system for covariance matrix, for absolute frames.

getCovRefLofType() - Method in class org.orekit.files.ccsds.OGMFile

Get coordinate system for covariance matrix, for Local Orbital Frames.

getCrc() - Method in class org.orekit.gnss.GPSAlmanac

getCrc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.

getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile

Get the file creation date and time in UTC.

getCreationDate() - Method in class org.orekit.files.ccsds.TDMFile

Get the file creation date and time in UTC.

getCrs() - Method in class org.orekit.gnss.GPSAlmanac

getCrs() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.

getCuc() - Method in class org.orekit.gnss.GPSAlmanac

getCuc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.

getCurrentDate() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the current date.

getCurrentDate() - Method in class org.orekit.estimation.sequential.KalmanEstimator

Get the current date.

getCurrentDate() - Method in class org.orekit.estimation.sequential.Model

Get the current date.

getCurrentMeasurementNumber() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the current measurement number.

getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.KalmanEstimator

Get the current measurement number.

getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.Model

Get the current measurement number.

getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Get the state at previous grid point date.

getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the state at current grid point date.

getCurrentWeight() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Deprecated.

as of 9.2, weight should not be changed anymore, rejected measurements are identified by their status

getCus() - Method in class org.orekit.gnss.GPSAlmanac

getCus() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.

getD() - Method in class org.orekit.data.DelaunayArguments

Get the mean elongation of the Moon from the Sun.

getD() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean elongation of the Moon from the Sun.

getDailyFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the daily F10.7 solar flux for previous day.

getDailyFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters

Get the value of the daily F10.7 solar flux for previous day.

getData() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the data valid during this time span.

getDataQuality() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the dataQuality.

getDataUsed() - Method in class org.orekit.files.sp3.SP3File

Returns the data used indicator from the SP3 file.

getDate() - Method in class org.orekit.attitudes.Attitude

Get the date of attitude parameters.

getDate() - Method in class org.orekit.attitudes.FieldAttitude

Get the date of attitude parameters.

getDate() - Method in class org.orekit.data.DelaunayArguments

Get the date.

getDate() - Method in class org.orekit.data.FieldDelaunayArguments

Get the date.

getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the date.

getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the date.

getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Get the date of the maneuver.

getDate() - Method in class org.orekit.frames.EOPEntry

Get the date.

getDate() - Method in class org.orekit.frames.FieldTransform

Get the date.

getDate() - Method in class org.orekit.frames.Transform

Get the date.

getDate() - Method in class org.orekit.gnss.DOP

Gets the calculation date of the DOP.

getDate() - Method in class org.orekit.gnss.GPSAlmanac

getDate() - Method in class org.orekit.gnss.ObservationDataSet

Get the date.

getDate() - Method in class org.orekit.orbits.FieldOrbit

Get the date of orbital parameters.

getDate() - Method in class org.orekit.orbits.Orbit

Get the date of orbital parameters.

getDate() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the TLE current date.

getDate() - Method in class org.orekit.propagation.events.DateDetector

Get the current event date according to the propagator.

getDate() - Method in class org.orekit.propagation.events.FieldDateDetector

Get the current event date according to the propagator.

getDate() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the date.

getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the date of the orbit.

getDate() - Method in class org.orekit.propagation.SpacecraftState

Get the date.

getDate() - Method in class org.orekit.time.AbsoluteDate

Get the date.

getDate() - Method in class org.orekit.time.DateTimeComponents

Get the date component.

getDate() - Method in class org.orekit.time.FieldAbsoluteDate

Get the date.

getDate() - Method in interface org.orekit.time.FieldTimeStamped

Get the date.

getDate() - Method in class org.orekit.time.GPSDate

Get the date.

getDate() - Method in interface org.orekit.time.TimeStamped

Get the date.

getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition

Get the transition absolute date.

getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the transition date.

getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Get the date.

getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Get the date.

getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Get the date.

getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates

Get the date.

getDay() - Method in class org.orekit.time.DateComponents

Get the day.

getDayFraction() - Method in class org.orekit.files.sp3.SP3File

Returns the day fraction for this SP3 file.

getDayOfWeek() - Method in class org.orekit.time.DateComponents

Get the day of week.

getDayOfYear() - Method in class org.orekit.time.DateComponents

Get the day number in year.

getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dC_j / dh coefficient.

getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dC_j / dk coefficient.

getDdEps() - Method in class org.orekit.frames.EOPEntry

Get the correction for nutation in obliquity δΔε.

getDDot() - Method in class org.orekit.data.DelaunayArguments

Get the mean elongation of the Moon from the Sun time derivative.

getDDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean elongation of the Moon from the Sun time derivative.

getDdPsi() - Method in class org.orekit.frames.EOPEntry

Get the correction for nutation in longitude δΔΨ.

getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField

Utility function to get a decimal year for a given day.

getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the declination of the magnetic field in degrees.

getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter

Get the decreasing events time shift.

getDefaultModel() - Static method in class org.orekit.models.earth.FixedTroposphericDelay

Returns the default model, loading delay values from the file "tropospheric-delay.txt".

getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide

Get the multipliers for Delaunay arguments (l, l', F, D, Ω).

getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get mass change during maneuver (value is < 0).

getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the velocity increment in satellite frame.

getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008

Get the local density with initial entries.

getDensity(int) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00.FieldOutput

Get one of the stored densities.

getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000

Get the local density with initial entries.

getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000

Get the local density with initial entries.

getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester

Get the local density.

getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester

Get the local density at some position.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester

Get the local density at some position.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere

getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008

Get the local density with initial entries.

getDepth() - Method in class org.orekit.frames.Frame

Get the depth of the frame.

getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the value of the derivative dK_j^{-n-1, s} / de².

getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Compute the value of the Hansen coefficient dK₀^{n, s} / dΧ.

getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Get the dK₀^-n-1,s / dΧ coefficient derivative.

getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Get Γ function derivative.

getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get all the drivers with set derivatives.

getDestination() - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Get the destination ITRF.

getDestination() - Method in class org.orekit.frames.ITRFVersion.Converter

Get the destination ITRF.

getDetector() - Method in class org.orekit.propagation.events.AdapterDetector

Get the wrapped detector.

getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event

Get the detector.

getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dα coefficient.

getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dβ coefficient.

getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dh coefficient.

getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dk coefficient.

getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_α coefficient.

getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_β coefficient.

getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_h coefficient.

getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_k coefficient.

getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dα coefficient.

getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dβ coefficient.

getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dh coefficient.

getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dk coefficient.

getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_α coefficient.

getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_β coefficient.

getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_h coefficient.

getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_k coefficient.

getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dα coefficient.

getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dβ coefficient.

getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dh coefficient.

getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dk coefficient.

getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the dimension of the measurement.

getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the dimension of the measurement.

getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the direction.

getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation

Get the displacement models.

getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dα coefficient.

getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dβ coefficient.

getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dh coefficient.

getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dk coefficient.

getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Get the value of dL_n^s / dγ (γ).

getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds

Get the upper bound value D_n^l(Χ).

getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Get the Doodson number for the wave.

getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide

Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).

getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide

Get the Doodson number.

getDragArea() - Method in class org.orekit.files.ccsds.OGMFile

Get the drag area.

getDragCoeff() - Method in class org.orekit.files.ccsds.OGMFile

Get the drag coefficient.

getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get the drivers for supported parameters.

getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive

Get the drivers for supported parameters.

getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag

Get the drivers for supported parameters.

getDrivers() - Method in class org.orekit.utils.ParameterDriversList

Get delegating drivers for all parameters.

getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType

Get parameters drivers initialized from a reference orbit.

getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dS_j / dh coefficient.

getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dS_j / dk coefficient.

getDSTDTC(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the temperature change computed from Dst index.

getDuration() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get duration (value is 0 for impulsive maneuver).

getDuration() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the duration of the maneuver (s).

getDV() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get velocity increment.

getDx() - Method in class org.orekit.frames.EOPEntry

Get the correction for Celestial Intermediate Pole (CIP) coordinates.

getDy() - Method in class org.orekit.frames.EOPEntry

Get the correction for Celestial Intermediate Pole (CIP) coordinates.

getE() - Method in class org.orekit.files.ccsds.OGMFile

Get the orbit eccentricity.

getE() - Method in class org.orekit.gnss.GPSAlmanac

getE() - Method in class org.orekit.orbits.CartesianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.Orbit

Get the eccentricity.

getE() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Eccentricity.

getE() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the eccentricity.

getE() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the eccentricity.

getE() - Method in class org.orekit.propagation.SpacecraftState

Get the eccentricity.

getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the earliest cached entry.

getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache

getEarliest() - Method in interface org.orekit.utils.TimeStampedCache

Get the earliest entry in this cache.

getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Earth singleton body.

getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Earth-Moon barycenter singleton bodies pair.

getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing the raw Earth Orientation Angle.

getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction to the east of point, expressed in parent shape frame.

getEast() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction to the east of point, expressed in parent shape frame.

getEast() - Method in class org.orekit.frames.TopocentricFrame

Get the east direction of topocentric frame, expressed in parent shape frame.

getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station position along East axis.

getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the eccentricity.

getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentric anomaly.

getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric anomaly.

getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentric anomaly derivative.

getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric anomaly derivative.

getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern

Get the phase center eccentricities.

getEccentricities() - Method in class org.orekit.gnss.RinexHeader

Get the eccentricities of antenna center.

getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna

Get the phase center eccentricities.

getECEF() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Gets the Earth Centered Earth Fixed frame used to propagate GPS orbits according to the GPS Interface Specification.

getECI() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Gets the Earth Centered Inertial frame used to propagate the orbit.

getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory

Get the ecliptic frame.

getEDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.Orbit

Get the eccentricity derivative.

getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the differential effects.

getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Get the value of an element.

getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the element number.

getElementSetNumber() - Method in class org.orekit.files.ccsds.OMMFile

Get the element set number for this satellite.

getElevation(double) - Method in class org.orekit.utils.ElevationMask

Get the interpolated elevation for a given azimuth according to the mask.

getElevation(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the elevation of a point with regards to the local point.

getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the elevation of a point with regards to the local point.

getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector

Get the elevation value.

getElevationMask() - Method in class org.orekit.gnss.DOPComputer

Get the elevation mask.

getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured elevation mask.

getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector

Returns the currently configured elevation mask.

getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape

Get the underlying ellipsoid model that defines latitude and longitude.

getEllipsoid() - Method in class org.orekit.models.earth.Geoid

getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid

getEME2000() - Static method in class org.orekit.frames.FramesFactory

Get the unique EME2000 frame.

getEnd() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the end of the measurements time span.

getEnd() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the end of this time span.

getEndDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the end date.

getEndDate() - Method in class org.orekit.frames.EOPHistory

Get the date of the last available Earth Orientation Parameters.

getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the total number of entries cached.

getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider

Get the EOP history.

getEOPHistory() - Method in class org.orekit.frames.GTODProvider

Get the EOP history.

getEOPHistory() - Method in class org.orekit.time.UT1Scale

Get the EOP history.

getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get Earth Orientation Parameters history.

getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions

Get the function computing tidal corrections for Earth Orientation Parameters.

getEphemeridesBlocks() - Method in class org.orekit.files.ccsds.OEMFile

Get the list of ephemerides blocks as an unmodifiable list.

getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get the ephemerides data lines comment.

getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile

Get the ephemeris type.

getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the type of ephemeris.

getEpoch() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix

Get the epoch relative to the covariance matrix.

getEpoch() - Method in class org.orekit.files.ccsds.OGMFile

Get epoch of state vector, Keplerian elements and covariance matrix data.

getEpoch() - Method in class org.orekit.files.ccsds.TDMFile.Observation

Getter for the epoch.

getEpoch() - Method in class org.orekit.files.sp3.SP3File

Returns the start epoch of the orbit file.

getEpoch() - Method in class org.orekit.frames.HelmertTransformation

Get the reference epoch of the transform.

getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the epoch for this magnetic field model.

getEpochComment() - Method in class org.orekit.files.ccsds.OGMFile

Get the comment for epoch.

getEpochIgnition() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get epoch ignition.

getEpochInterval() - Method in class org.orekit.files.sp3.SP3File

Returns the time interval between epochs (in seconds).

getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the equatorial radius of the body.

getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Get the central body equatorial radius.

getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.orbits.Orbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the first component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState

Get the first component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.orbits.Orbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the second component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState

Get the second component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit

Get the second component of the equinoctial eccentricity vector.

getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for equinox-based paradigm.

getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for equinox-based paradigm.

getEstimate() - Method in class org.orekit.estimation.sequential.Model

Get the current corrected estimate.

getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation

Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.

getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider

Get one estimated measurement.

getEstimatedMeasurementsParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the list of estimated measurements parameters.

getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.KalmanEstimator

Get the list of estimated measurements parameters.

getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.Model

Get the list of estimated measurements parameters.

getEstimatedOrbitalParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the list of estimated orbital parameters.

getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.Model

Get the list of estimated orbital parameters.

getEstimatedPropagationParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the list of estimated propagation parameters.

getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.Model

Get the list of estimated propagation parameters.

getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.Model

Get the propagators estimated with the values set in the propagators builders.

getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get the estimated UT1 time scale.

getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation

Get the estimated UT1 scale, including the estimated linear models for prime meridian.

getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the estimated value.

getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the number of objective function evaluations.

getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the number of evaluations used for last estimation.

getEventDate() - Method in class org.orekit.propagation.events.EventState

Get the occurrence time of the event triggered in the current step.

getEventDate() - Method in class org.orekit.propagation.events.FieldEventState

Get the occurrence time of the event triggered in the current step.

getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the event detector triggered.

getEventDetector() - Method in class org.orekit.propagation.events.EventState

Get the underlying event detector.

getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent

Get the event detector triggered.

getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState

Get the underlying event detector.

getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue

Get the events passed to this handler.

getEventsDetectors() - Method in class org.orekit.forces.AbstractParametricAcceleration

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce

Get the discrete events related to the model.

getEventsDetectors() - Method in interface org.orekit.forces.ForceModel

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in interface org.orekit.propagation.Propagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get the discrete events related to the model.

getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Get the discrete events related to the model.

getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.Model

getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper

Deprecated.

Get the wrapped exception.

getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris

Get the maximum timespan outside of the stored ephemeris that is allowed for extrapolation.

getF() - Method in class org.orekit.data.DelaunayArguments

Get L - Ω where L is the mean longitude of the Moon.

getF() - Method in class org.orekit.data.FieldDelaunayArguments

Get L - Ω where L is the mean longitude of the Moon.

getF10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).

getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the value of the mean solar flux.

getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame

Get the key of the frame within the factory.

getFDot() - Method in class org.orekit.data.DelaunayArguments

Get L - Ω where L is the mean longitude of the Moon time derivative.

getFDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get L - Ω where L is the mean longitude of the Moon time derivative.

getField() - Method in class org.orekit.propagation.FieldAbstractPropagator

Field getter.

getField() - Method in class org.orekit.time.FieldAbsoluteDate

Get the field.

getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory

Get the GeoMagneticField for the given model type and year.

getFieldDate() - Method in class org.orekit.frames.FieldTransform

Get the date.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.AbstractParametricAcceleration

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.DragForce

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.Relativity

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the discrete events related to the model.

getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the discrete events related to the model.

getFieldOfView() - Method in class org.orekit.propagation.events.FieldOfViewDetector

Get the Field Of View.

getFieldOfView() - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Get the Field Of View.

getFieldOfView() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector

Get the Field Of View.

getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the magnetic field vector in nTesla.

getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.

getFileDate(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the date of the file from which data at the specified date comes from.

getFileFormat() - Method in class org.orekit.files.ccsds.TDMParser

Get file format.

getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter

Get the filter corresponding to a maximum derivation order.

getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter

Get the filter corresponding to a maximum derivation order.

getFirst() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Get the first TLE.

getFirstDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Get the start date of the series.

getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale

Get the date of the first known leap second.

getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic

Get a copy of the last fitted parameters.

getFixedStepSize() - Method in class org.orekit.propagation.AbstractPropagator

Get the fixed step size.

getFixedStepSize() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the fixed step size.

getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the flattening of the body: f = (a-b)/a.

getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the flow rate.

getForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Deprecated.

as of 9.1, this method is deprecated, the perturbing force models are retrieved together with the Newtonian attraction by calling FieldNumericalPropagator.getAllForceModels()

getFormatVersion() - Method in class org.orekit.files.ccsds.ODMFile

Get the CCSDS ODM (OPM, OMM or OEM) format version.

getFormatVersion() - Method in class org.orekit.files.ccsds.TDMFile

Get the CCSDS TDM format version.

getFrame() - Method in class org.orekit.bodies.Ellipse

Get the defining frame.

getFrame() - Method in class org.orekit.bodies.Ellipsoid

Get the ellipsoid central frame.

getFrame() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).

getFrame() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix

Get coordinate system for covariance matrix, for absolute frames.

getFrame() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the reference frame for this ephemeris segment.

getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getFrame() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getFrame() - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.atmosphere.DTM2000

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.atmosphere.JB2008

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere

Get the frame of the central body.

getFrame() - Method in class org.orekit.frames.OrphanFrame

Get the associated frame.

getFrame() - Method in class org.orekit.orbits.FieldOrbit

Get the frame in which the orbital parameters are defined.

getFrame() - Method in class org.orekit.orbits.Orbit

Get the frame in which the orbital parameters are defined.

getFrame() - Method in class org.orekit.propagation.AbstractPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris

getFrame() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the frame of the initial state.

getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector

Get the frame in which the equator is defined.

getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector

Get the sensor reference frame.

getFrame() - Method in class org.orekit.propagation.events.NodeDetector

Get the frame in which the equator is defined.

getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in interface org.orekit.propagation.FieldPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the inertial frame.

getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get the inertial frame.

getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris

getFrame() - Method in class org.orekit.propagation.integration.StateMapper

Get the inertial frame.

getFrame() - Method in interface org.orekit.propagation.Propagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the definition frame of the orbit.

getFrame() - Method in class org.orekit.propagation.SpacecraftState

Get the inertial frame.

getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory

Get one of the predefined frames.

getFrame(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame

Get the frame corresponding to the CCSDS constant.

getFrameCenterString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getFrameCenterString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the name of the center of the coordinate system the ephemeris is provided in.

getFrameCenterString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getFrameCenterString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getFrameEpoch() - Method in class org.orekit.files.ccsds.ODMMetaData

Get epoch of reference frame, if not intrinsic to the definition of the reference frame.

getFrameEpochString() - Method in class org.orekit.files.ccsds.ODMMetaData

Get epoch of reference frame, if not intrinsic to the definition of the reference frame.

getFrameString() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the reference frame specifier as it appeared in the file.

getFrameString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getFrameString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the defining frame for this ephemeris segment.

getFrameString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getFrameString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter

Get the number of free state parameters.

getFreqOffset() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the freqOffset.

getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType

Get the frequency for a specified satellite system.

getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame

Get a new version of the instance, frozen with respect to a reference frame.

getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector

Get the switching function.

getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Dummy date at infinity in the future direction.

getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.

getGamma() - Method in class org.orekit.data.DelaunayArguments

Get the tide parameter γ = GMST + π.

getGamma() - Method in class org.orekit.data.FieldDelaunayArguments

Get the tide parameter γ = GMST + π.

getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get direction cosine γ for central body.

getGammaDot() - Method in class org.orekit.data.DelaunayArguments

Get the tide parameter γ = GMST + π time derivative.

getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the tide parameter γ = GMST + π time derivative.

getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich apparent sidereal time, in radians.

getGCRF() - Static method in class org.orekit.frames.FramesFactory

Get the unique GCRF frame.

getGdop() - Method in class org.orekit.gnss.DOP

Gets the geometric dilution of precision.

getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of calls to the generate method.

getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator

Get the ephemeris generated during propagation.

getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Get the ephemeris generated during propagation.

getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Get the ephemeris generated during propagation.

getGeneratedEphemeris() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the ephemeris generated during propagation.

getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldPropagator

Get the ephemeris generated during propagation.

getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the ephemeris generated during propagation.

getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the ephemeris generated during propagation.

getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator

Get the ephemeris generated during propagation.

getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the generator.

getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.

getGFunction() - Method in class org.orekit.propagation.events.FunctionalDetector

Deprecated.

use FunctionalDetector.getFunction() instead. Will be removed in next major release.

getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the G_js coefficient.

getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory

Get the GLObal NAvigation Satellite System time scale.

getGM() - Method in interface org.orekit.bodies.CelestialBody

Get the attraction coefficient of the body.

getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid

Gets the gravitational parameter that is part of the definition of the reference ellipsoid.

getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the G_ms^j coefficient.

getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory

Get the Greenwich Mean Sidereal Time scale.

getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich mean sidereal time, in radians.

getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich mean sidereal time rate, in radians per second.

getGnssNb() - Method in class org.orekit.gnss.DOP

Gets the number of GNSS satellites taken into account for DOP computation.

getGPS() - Static method in class org.orekit.time.TimeScalesFactory

Get the Global Positioning System scale.

getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.

getGPSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Gets the underlying GPS orbital elements.

getGpsWeek() - Method in class org.orekit.files.sp3.SP3File

Returns the GPS week as contained in the SP3 file.

getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the number of interpolation grid points.

getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider

Get the number of interpolation grid points.

getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid

Get grid points that are within the current step.

getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid

Get grid points that are within the current step.

getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid

Get grid points that are within the current step.

getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid

Get the GRS80 ellipsoid, attached to the given body frame.

getGST() - Static method in class org.orekit.time.TimeScalesFactory

Get the Galileo System Time scale.

getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory

Get the GTOD reference frame.

getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the GTOD reference frame.

getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the y component of eccentricity vector.

getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector

Get FOV half aperture angle.

getHandler() - Method in class org.orekit.propagation.events.AbstractDetector

Get the handler.

getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Get the handler.

getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic

Get an upper bound of the fitted harmonic amplitude.

getHasCreatableBody() - Method in class org.orekit.files.ccsds.ODMMetaData

Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodyFactory.

getHasManeuver() - Method in class org.orekit.files.ccsds.OPMFile

Get boolean testing whether the OPM contains at least one maneuver.

getHasRefFrameEpoch() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get boolean testing whether the reference frame has an epoch associated to it.

getHdop() - Method in class org.orekit.gnss.DOP

Gets the horizontal dilution of precision.

getHeader() - Method in class org.orekit.gnss.ObservationDataSet

Get the Rinex header associated with this data set.

getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile

Get the header comment.

getHeaderComment() - Method in class org.orekit.files.ccsds.TDMFile

Get the header comment.

getHealth() - Method in class org.orekit.gnss.GPSAlmanac

Gets the Health status.

getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the H_js coefficient.

getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the H_ms^j coefficient.

getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).

getHour() - Method in class org.orekit.time.TimeComponents

Get the hour number.

getHx() - Method in class org.orekit.orbits.CartesianOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.KeplerianOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.Orbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the first component of the inclination vector (as per equinoctial parameters).

getHx() - Method in class org.orekit.propagation.SpacecraftState

Get the first component of the inclination vector (as per equinoctial parameters).

getHxDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.Orbit

Get the first component of the inclination vector derivative.

getHy() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.KeplerianOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.Orbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the second component of the inclination vector (as per equinoctial parameters).

getHy() - Method in class org.orekit.propagation.SpacecraftState

Get the second component of the inclination vector (as per equinoctial parameters).

getHyDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.Orbit

Get the second component of the inclination vector derivative.

getI() - Method in class org.orekit.files.ccsds.OGMFile

Get the orbit inclination.

getI() - Method in class org.orekit.orbits.CartesianOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.CircularOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.KeplerianOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.Orbit

Get the inclination.

getI() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the inclination.

getI() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the inclination.

getI() - Method in class org.orekit.propagation.SpacecraftState

Get the inclination.

getI0() - Method in class org.orekit.gnss.GPSAlmanac

getI0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Inclination Angle at Reference Time.

getICRF() - Static method in class org.orekit.frames.FramesFactory

Get the unique ICRF frame.

getId() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris

getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

getId() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform

Get the identity transform.

getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates

Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).

getIDot() - Method in class org.orekit.gnss.GPSAlmanac

getIDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.CircularOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.Orbit

Get the inclination derivative.

getIDot() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Rate of Inclination Angle.

getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory

Get the IGRF model for the given year.

getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the I_js coefficient.

getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers

Get the imaginary part of a nominal Love numbers.

getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the inclination of the magnetic field in degrees.

getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter

Get the increasing events time shift.

getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Get the inertial velocity increment of the maneuver.

getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Get the inertial frame in which the velocity increment is defined.

getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody

Get an inertially oriented, body centered frame.

getInitialCovarianceMatrix(SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider

Get the initial covariance matrix.

getInitialCovarianceMatrix(SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider

Get the initial covariance matrix.

getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the initial state for integration.

getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the initial state for integration.

getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the initial state for integration.

getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the date of the initial orbit.

getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the date of the initial orbit.

getInitialState() - Method in class org.orekit.propagation.AbstractPropagator

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the propagator initial state.

getInitialState() - Method in interface org.orekit.propagation.FieldPropagator

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the propagator initial state.

getInitialState() - Method in interface org.orekit.propagation.Propagator

Get the propagator initial state.

getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.Model

getInstance() - Static method in class org.orekit.data.DataProvidersManager

Get the unique instance.

getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the instantaneous solar flux.

getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters

Get the value of the instantaneous solar flux.

getIntegrationInterval() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the integrationInterval.

getIntegrationRef() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the integrationRef.

getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the integrator used by the propagator.

getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the integrator used by the propagator.

getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Get the integrator builder.

getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile

Get an interpolated point inside the tile.

getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the state at interpolated date.

getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Get the state at interpolated date.

getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get the interpolation degree.

getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get the interpolation method to be used.

getInterpolationSamples() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid

Get the intersection point of a line with the surface of the body.

getInterval() - Method in class org.orekit.gnss.RinexHeader

Get the observation interval in seconds.

getInverse() - Method in class org.orekit.frames.FieldTransform

Get the inverse transform of the instance.

getInverse() - Method in class org.orekit.frames.Transform

Get the inverse transform of the instance.

getIODC() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Issue Of Data Clock (IODC).

getIODE() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Issue Of Data Ephemeris (IODE).

getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory

Get the Indian Regional Navigation Satellite System time scale.

getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the specific impulse.

getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the specific impulse.

getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the iteration number.

getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the number of iterations used for last estimation.

getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get an specific International Terrestrial Reference Frame.

getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get an unspecified International Terrestrial Reference Frame.

getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the equinox-based ITRF reference frame.

getITRFType() - Method in class org.orekit.frames.EOPEntry

Get the ITRF version this entry defines.

getITRFVersion() - Method in class org.orekit.frames.VersionedITRF

Get the ITRF version.

getITRFVersion(int) - Static method in enum org.orekit.frames.ITRFVersion

Find an ITRF version from its reference year.

getITRFVersion(String) - Static method in enum org.orekit.frames.ITRFVersion

Find an ITRF version from its name.

getITRFVersion(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the ITRF version.

getJ2000Day() - Method in class org.orekit.time.DateComponents

Get the day number with respect to J2000 epoch.

getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).

getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the Jacobian of the orbit with respect to maneuver parameters.

getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform

Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.

getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform

Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.

getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.

getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.

getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.

getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.

getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.

getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the J_js coefficient.

getJulianDay() - Method in class org.orekit.files.sp3.SP3File

Returns the julian day for this SP3 file.

getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.

getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Jupiter singleton body.

getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the x component of eccentricity vector.

getKeplerianElementsComment() - Method in class org.orekit.files.ccsds.OGMFile

Get the comment for Keplerian elements.

getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit

Get the Keplerian mean motion.

getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit

Get the Keplerian mean motion.

getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the Keplerian mean motion.

getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState

Get the Keplerian mean motion.

getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState

Get the Keplerian period.

getKey() - Method in enum org.orekit.gnss.SatelliteSystem

Get the key for the system.

getKeyword() - Method in class org.orekit.files.ccsds.TDMFile.Observation

Getter for the keyword.

getL() - Method in class org.orekit.data.DelaunayArguments

Get the mean anomaly of the Moon.

getL() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean anomaly of the Moon.

getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit

Get the longitude argument.

getL(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the longitude argument.

getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Get the last TLE.

getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Get the last date of the series.

getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the last estimations performed.

getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale

Get the date of the last known leap second.

getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the latest cached entry.

getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache

getLatest() - Method in interface org.orekit.utils.TimeStampedCache

Get the latest entry in this cache.

getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the latitude.

getLatitude() - Method in class org.orekit.bodies.GeodeticPoint

Get the latitude.

getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector

Get the fixed latitude to be crossed (radians).

getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the launch number.

getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMParser

Get the launch number.

getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the launch number.

getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the piece of launch.

getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMParser

Get the piece of launch.

getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the launch piece.

getLaunchYear() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the launch year.

getLaunchYear() - Method in class org.orekit.files.ccsds.ODMParser

Get the launch year.

getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the launch year.

getLDot() - Method in class org.orekit.data.DelaunayArguments

Get the mean anomaly of the Moon time derivative.

getLDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean anomaly of the Moon time derivative.

getLDot(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit

Get the longitude argument derivative.

getLDot(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the longitude argument derivative.

getLE() - Method in class org.orekit.data.BodiesElements

Get the mean Earth longitude.

getLE() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Earth longitude.

getLE() - Method in class org.orekit.orbits.CartesianOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.Orbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the eccentric latitude argument (as per equinoctial parameters).

getLE() - Method in class org.orekit.propagation.SpacecraftState

Get the eccentric longitude argument (as per equinoctial parameters).

getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale

Get the value of the previous leap.

getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Get the value of the previous leap.

getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Get the value of the previous leap.

getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale

Get the value of the previous leap.

getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale

Get the value of the previous leap.

getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale

Get the value of the previous leap.

getLeapSeconds() - Method in class org.orekit.gnss.RinexHeader

Get the Number of leap seconds since 6-Jan-1980.

getLeapSecondsDayNum() - Method in class org.orekit.gnss.RinexHeader

Get the respective leap second day number.

getLeapSecondsFuture() - Method in class org.orekit.gnss.RinexHeader

Get the future or past leap seconds.

getLeapSecondsWeekNum() - Method in class org.orekit.gnss.RinexHeader

Get the respective leap second week number.

getLEDot() - Method in class org.orekit.data.BodiesElements

Get the mean Earth longitude time derivative.

getLEDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Earth longitude time derivative.

getLEDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.Orbit

Get the eccentric longitude argument derivative.

getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the eccentric longitude.

getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the lighting ratio ([0-1]).

getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the lighting ratio ([0-1]).

getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the first line.

getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the second line.

getListAppliedDCBS() - Method in class org.orekit.gnss.RinexHeader

Get the list of applied differential code bias corrections.

getListAppliedPCVS() - Method in class org.orekit.gnss.RinexHeader

Get the list of antenna center variation corrections.

getLJu() - Method in class org.orekit.data.BodiesElements

Get the mean Jupiter longitude.

getLJu() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Jupiter longitude.

getLJuDot() - Method in class org.orekit.data.BodiesElements

Get the mean Jupiter longitude time derivative.

getLJuDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Jupiter longitude time derivative.

getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Compute the limits in L, the true longitude, for integration.

getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Compute the limits in L, the true longitude, for integration.

getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Compute the limits in L, the true longitude, for integration.

getLM() - Method in class org.orekit.orbits.CartesianOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.CircularOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.KeplerianOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.Orbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the mean latitude argument (as per equinoctial parameters).

getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the mean longitude.

getLM() - Method in class org.orekit.propagation.SpacecraftState

Get the mean longitude argument (as per equinoctial parameters).

getLMa() - Method in class org.orekit.data.BodiesElements

Get the mean Mars longitude.

getLMa() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Mars longitude.

getLMaDot() - Method in class org.orekit.data.BodiesElements

Get the mean Mars longitude time derivative.

getLMaDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Mars longitude time derivative.

getLMDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.CircularOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.Orbit

Get the mean longitude argument derivative.

getLMe() - Method in class org.orekit.data.BodiesElements

Get the mean Mercury longitude.

getLMe() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Mercury longitude.

getLMeDot() - Method in class org.orekit.data.BodiesElements

Get the mean Mercury longitude time derivative.

getLMeDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Mercury longitude time derivative.

getLNe() - Method in class org.orekit.data.BodiesElements

Get the mean Neptune longitude.

getLNe() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Neptune longitude.

getLNeDot() - Method in class org.orekit.data.BodiesElements

Get the mean Neptune longitude time derivative.

getLNeDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Neptune longitude time derivative.

getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Get the value of L_n^s(γ).

getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get astronomical unit.

getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get a constant defined in the ephemerides headers.

getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager

Get an unmodifiable view of the set of data file names that have been loaded.

getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get Earth/Moon mass ratio.

getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get the gravitational coefficient of a body.

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIOException

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException

getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages

getLocation() - Method in class org.orekit.gnss.DOP

Gets the location with respect to the Earth where DOP was calculated.

getLOD() - Method in class org.orekit.frames.EOPEntry

Get the LoD (Length of Day) value.

getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the LoD (Length of Day) value.

getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the LoD (Length of Day) value.

getLofCartesianOrbitalParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the lofCartesianOrbitalParametersEvolution.

getLofType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the lofType.

getLofType() - Method in enum org.orekit.files.ccsds.CCSDSFrame

Get the type of Local Orbital frame.

getLofType() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix

Get coordinate system for covariance matrix, for Local Orbital Frames.

getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger

Get an immutable copy of the logged events.

getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger

Get an immutable copy of the logged events.

getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the longitude.

getLongitude() - Method in class org.orekit.bodies.GeodeticPoint

Get the longitude.

getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Get the fixed longitude to be crossed (radians).

getLossOfLockIndicator() - Method in class org.orekit.gnss.ObservationData

Get the Loss of Lock Indicator.

getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions

Get the Love numbers.

getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month

Get the lower case three letters abbreviation.

getLowerCaseName() - Method in enum org.orekit.time.Month

Get the lower case full name.

getLPrime() - Method in class org.orekit.data.DelaunayArguments

Get the mean anomaly of the Sun.

getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean anomaly of the Sun.

getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments

Get the mean anomaly of the Sun time derivative.

getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean anomaly of the Sun time derivative.

getLSa() - Method in class org.orekit.data.BodiesElements

Get the mean Saturn longitude.

getLSa() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Saturn longitude.

getLSaDot() - Method in class org.orekit.data.BodiesElements

Get the mean Saturn longitude time derivative.

getLSaDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Saturn longitude time derivative.

getLUr() - Method in class org.orekit.data.BodiesElements

Get the mean Uranus longitude.

getLUr() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Uranus longitude.

getLUrDot() - Method in class org.orekit.data.BodiesElements

Get the mean Uranus longitude time derivative.

getLUrDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Uranus longitude time derivative.

getLv() - Method in class org.orekit.orbits.CartesianOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.CircularOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.KeplerianOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.Orbit

Get the true longitude argument.

getLv() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the true latitude argument (as per equinoctial parameters).

getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the true longitude.

getLv() - Method in class org.orekit.propagation.SpacecraftState

Get the true longitude argument (as per equinoctial parameters).

getLvDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.CircularOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.Orbit

Get the true longitude argument derivative.

getLVe() - Method in class org.orekit.data.BodiesElements

Get the mean Venus longitude.

getLVe() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Venus longitude.

getLVeDot() - Method in class org.orekit.data.BodiesElements

Get the mean Venus longitude time derivative.

getLVeDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Venus longitude time derivative.

getM0() - Method in class org.orekit.gnss.GPSAlmanac

getM0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Mean Anomaly at Reference Time.

getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the differential equations to integrate (for main state only).

getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris

Get all the names of all managed states.

getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator

Get all the names of all managed states.

getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile

Get a maneuver.

getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile

Get a list of all maneuvers.

getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Get a mapper between two-dimensional Jacobians and one-dimensional additional state.

getMargin() - Method in class org.orekit.propagation.events.FieldOfView

Get the angular margin to apply (radians).

getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector

Get the angular margin to apply (radians).

getMarkerName() - Method in class org.orekit.gnss.RinexHeader

Get name of the antenna marker.

getMarkerNumber() - Method in class org.orekit.gnss.RinexHeader

Get number of the antenna marker.

getMarkerType() - Method in class org.orekit.gnss.RinexHeader

Get type of the antenna marker.

getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Mars singleton body.

getMass() - Method in class org.orekit.files.ccsds.OGMFile

Get the spacecraft mass.

getMass() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Get the mass.

getMass() - Method in class org.orekit.propagation.FieldSpacecraftState

Gets the current mass.

getMass() - Method in class org.orekit.propagation.SpacecraftState

Gets the current mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the mass.

getMasterStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange

Get the master ground station from which measurement is performed.

getMatrix() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix

Get the covariance matrix.

getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Get a line of the matrix.

getMaxAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester

Get the maximal altitude for the model.

getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the maximal degree available in the last file parsed.

getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the maximal order available in the last file parsed.

getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in class org.orekit.propagation.events.AdapterDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector

Get maximal time interval between switching function checks.

getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get the maximal chunks duration.

getMaxDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Gets the available data range maximum date.

getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters

Gets the available data range maximum date.

getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Gets the available data range maximum date.

getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters

Gets the available data range maximum date.

getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris

Get the last date of the range.

getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator

Get the last date of the range.

getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator

Get the last date of the range.

getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the last date of the range.

getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the last date of the range.

getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the maximal supported degree.

getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Get the maximum supported degree.

getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the maximal supported degree.

getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in class org.orekit.propagation.events.AdapterDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector

Get maximal number of iterations in the event time search.

getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the maximal supported order.

getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Get the maximum supported order.

getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the maximal supported order.

getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter

Get the maximum derivation order.

getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter

Get the maximum derivation order.

getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the degree limit for the next file parsing.

getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the degree limit for the next file parsing.

getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the order limit for the next file parsing.

getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the order limit for the next file parsing.

getMaxSigma() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter

Get the value of the outlier detection limit.

getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the maximum number of independent cached time slots.

getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the maximum duration span in seconds of one slot.

getMaxValue() - Method in class org.orekit.utils.ParameterDriver

Get maximum parameter value.

getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the mean anomaly.

getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit

Get the mean anomaly.

getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the mean anomaly.

getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the mean anomaly derivative.

getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the mean anomaly derivative.

getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementTheory() - Method in class org.orekit.files.ccsds.OMMFile.OMMMetaData

Get the description of the Mean Element Theory.

getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the mean solar flux.

getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters

Get the value of the mean solar flux.

getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile

Get the orbit mean motion.

getMeanMotion() - Method in class org.orekit.gnss.GPSAlmanac

getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Mean Motion.

getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the Keplerian mean motion.

getMeanMotionDot() - Method in class org.orekit.files.ccsds.OMMFile

Get the first time derivative of the mean motion.

getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.OMMFile

Get the second time derivative of the mean motion.

getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the mean motion first derivative.

getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the mean motion second derivative.

getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions

Get the function computing mean obliquity of the ecliptic.

getMeasurement() - Method in class org.orekit.files.ccsds.TDMFile.Observation

Getter for the measurement.

getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the measurements parameters supported by this estimator (including measurements and modifiers).

getMeasurementType() - Method in enum org.orekit.gnss.ObservationType

Get the measurement type.

getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Mercury singleton body.

getMessage() - Method in exception org.orekit.errors.OrekitException

getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException

getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException

getMessage() - Method in exception org.orekit.errors.OrekitInternalError

getMessage() - Method in exception org.orekit.errors.OrekitIOException

getMessage() - Method in exception org.orekit.errors.OrekitParseException

getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException

Gets the message in a specified locale.

getMessage(Locale) - Method in exception org.orekit.errors.OrekitException

Gets the message in a specified locale.

getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException

Gets the message in a specified locale.

getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException

Gets the message in a specified locale.

getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError

Gets the message in a specified locale.

getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException

Gets the message in a specified locale.

getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException

Gets the message in a specified locale.

getMetaData() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get the meta-data for the block.

getMetaData() - Method in class org.orekit.files.ccsds.OGMFile

Get the meta data.

getMetaData() - Method in class org.orekit.files.ccsds.OMMFile

Get the meta data.

getMetaData() - Method in class org.orekit.files.ccsds.OPMFile

Get the meta data.

getMetaData() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Get the meta-data for the block.

getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile

Get the comment for meta-data.

getMHzFrequency() - Method in enum org.orekit.gnss.Frequency

Get the value of the frequency in MHz.

getMilliInWeek() - Method in class org.orekit.time.GPSDate

Get the number of milliseconds since week start.

getMinAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester

Get the minimal altitude for the model.

getMinDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Gets the available data range minimum date.

getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters

Gets the available data range minimum date.

getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Gets the available data range minimum date.

getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters

Gets the available data range minimum date.

getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris

Get the first date of the range.

getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator

Get the first date of the range.

getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator

Get the first date of the range.

getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the first date of the range.

getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the first date of the range.

getMinElevation() - Method in class org.orekit.gnss.DOPComputer

Get the minimum elevation.

getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured minimum valid elevation value.

getMinElevation() - Method in class org.orekit.propagation.events.FieldElevationDetector

Returns the currently configured minimum valid elevation value.

getMinute() - Method in class org.orekit.time.TimeComponents

Get the minute number.

getMinutesFromUTC() - Method in class org.orekit.time.TimeComponents

Get the offset between the specified date and UTC.

getMinValue() - Method in class org.orekit.utils.ParameterDriver

Get minimum parameter value.

getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMFile

Get reference date for Mission Elapsed Time and Mission Relative Time time systems.

getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMParser

Get initial date.

getMissionReferenceDate() - Method in class org.orekit.files.ccsds.TDMParser

Get initial date.

getMjd() - Method in class org.orekit.frames.EOPEntry

Get the entry date (modified julian day, 00h00 UTC scale).

getMJD() - Method in class org.orekit.time.DateComponents

Get the modified julian day.

getMJDRef() - Method in class org.orekit.time.OffsetModel

Get the reference date of the linear model as a modified julian day.

getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory

Get the MOD reference frame.

getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory

Get the MOD reference frame.

getMode() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the mode.

getMode() - Method in class org.orekit.propagation.AbstractPropagator

Get the current operating mode of the propagator.

getMode() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the current operating mode of the propagator.

getMode() - Method in interface org.orekit.propagation.FieldPropagator

Get the current operating mode of the propagator.

getMode() - Method in interface org.orekit.propagation.Propagator

Get the current operating mode of the propagator.

getModel() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the Jacobian of the function computing position/velocity at sample points.

getModel() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter

Get the Jacobian of the function computing position/velocity at sample points.

getModel() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter

Get the Jacobian of the function computing position/velocity at sample points.

getModelName() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the model name.

getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Returns a Collection of the GeoMagneticField models that have been successfully loaded.

getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.

getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates

Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.

getModifiedRodrigues(double) - Method in class org.orekit.utils.FieldAngularCoordinates

Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.

getModifiers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the modifiers that apply to a measurement.

getModifiers() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the modifiers that apply to a measurement.

getModifiers() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Get the modifiers that apply to a measurement.

getModifiers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the modifiers that apply to a measurement.

getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates

Gets the momentum.

getMomentum() - Method in class org.orekit.utils.PVCoordinates

Gets the momentum.

getMonth() - Method in class org.orekit.time.DateComponents

Get the month.

getMonth(int) - Static method in enum org.orekit.time.Month

Get the month corresponding to a number.

getMonthEnum() - Method in class org.orekit.time.DateComponents

Get the month as an enumerate.

getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Moon singleton body.

getMu() - Method in class org.orekit.files.ccsds.ODMParser

Get gravitational coefficient.

getMu() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getMu() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris

getMu() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the standard gravitational parameter for the satellite.

getMu() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

getMu() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getMu() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.forces.gravity.NewtonianAttraction

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the central body attraction coefficient.

getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the central body attraction coefficient.

getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the central body attraction coefficient.

getMu() - Method in class org.orekit.orbits.FieldOrbit

getMu() - Method in class org.orekit.orbits.Orbit

Get the central acceleration constant.

getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the central attraction coefficient (µ - m³/s²) value.

getMu() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the central attraction coefficient.

getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.integration.StateMapper

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the central body attraction coefficient.

getMu() - Method in class org.orekit.propagation.SpacecraftState

Get the central attraction coefficient.

getMU() - Static method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Get the Earth gravity coefficient used for GPS propagation.

getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the Earth gravity coefficient used for TLE propagation.

getMuCreated() - Method in class org.orekit.files.ccsds.ODMFile

Get the gravitational coefficient created from the knowledge of the central body.

getMuParsed() - Method in class org.orekit.files.ccsds.ODMFile

Get the gravitational coefficient parsed in the ODM File.

getMuSet() - Method in class org.orekit.files.ccsds.ODMFile

Get the gravitational coefficient set by the user.

getMuUsed() - Method in class org.orekit.files.ccsds.ODMFile

Get the used gravitational coefficient.

getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

Get n.

getNadir() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction below the point, expressed in parent shape frame.

getNadir() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction below the point, expressed in parent shape frame.

getNadir() - Method in class org.orekit.frames.TopocentricFrame

Get the nadir direction of topocentric frame, expressed in parent shape frame.

getName() - Method in interface org.orekit.bodies.CelestialBody

Get the name of the body.

getName() - Method in class org.orekit.data.NamedData

Get the name of the data.

getName() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the name.

getName() - Method in class org.orekit.frames.Frame

Get the name.

getName() - Method in enum org.orekit.frames.ITRFVersion

Get the name the frame version.

getName() - Method in enum org.orekit.frames.Predefined

Get the name of the frame.

getName() - Method in enum org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

Get the IGS name for the antenna code.

getName() - Method in enum org.orekit.gnss.antenna.SatelliteType

Get the IGS name for the antenna code.

getName() - Method in enum org.orekit.gnss.Frequency

Get the RINEX name for the frequency.

getName() - Method in interface org.orekit.propagation.AdditionalStateProvider

Get the name of the additional state.

getName() - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider

Get the name of the additional state.

getName() - Method in interface org.orekit.propagation.FieldAdditionalStateProvider

Get the name of the additional state.

getName() - Method in interface org.orekit.propagation.integration.AdditionalEquations

Get the name of the additional state.

getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations

Get the name of the additional state.

getName() - Method in class org.orekit.propagation.numerical.JacobiansMapper

Get the name of the partial Jacobians.

getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Get the name of the additional state.

getName() - Method in class org.orekit.time.BDTScale

Get the name time scale.

getName() - Method in class org.orekit.time.GalileoScale

Get the name time scale.

getName() - Method in class org.orekit.time.GLONASSScale

Get the name time scale.

getName() - Method in class org.orekit.time.GMSTScale

Get the name time scale.

getName() - Method in class org.orekit.time.GPSScale

Get the name time scale.

getName() - Method in class org.orekit.time.IRNSSScale

Get the name time scale.

getName() - Method in class org.orekit.time.QZSSScale

Get the name time scale.

getName() - Method in class org.orekit.time.TAIScale

Get the name time scale.

getName() - Method in class org.orekit.time.TCBScale

Get the name time scale.

getName() - Method in class org.orekit.time.TCGScale

Get the name time scale.

getName() - Method in class org.orekit.time.TDBScale

Get the name time scale.

getName() - Method in interface org.orekit.time.TimeScale

Get the name time scale.

getName() - Method in class org.orekit.time.TTScale

Get the name time scale.

getName() - Method in class org.orekit.time.UT1Scale

Get the name time scale.

getName() - Method in class org.orekit.time.UTCScale

Get the name time scale.

getName() - Method in class org.orekit.utils.ParameterDriver

Get name.

getNbManeuvers() - Method in class org.orekit.files.ccsds.OPMFile

Get the number of maneuvers present in the OPM.

getNbParams() - Method in class org.orekit.utils.ParameterDriversList

Get the number of parameters with different names.

getNbSpecies() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the number of species.

getNbTides(int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the number of tides for one species.

getNeighbors(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the entries surrounding a central date.

getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.GenericTimeStampedCache

Get the entries surrounding a central date.

getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.ImmutableTimeStampedCache

Get the entries surrounding a central date.

getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache

Get the entries surrounding a central date.

getNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the fixed size of the arrays to be returned by GenericTimeStampedCache.getNeighbors(AbsoluteDate).

getNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache

getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache

Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).

getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Neptune singleton body.

getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache

Get quantum gap above which a new slot is created instead of extending an existing one.

getNewState() - Method in class org.orekit.propagation.events.EventState.EventOccurrence

Get the new state for a reset action.

getNewState() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence

Get the new state for a reset action.

getNewtonianAttractionForceModel() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Deprecated.

as of 9.1, this method is deprecated, the Newtonian attraction force model (if any) is the last in the FieldNumericalPropagator.getAllForceModels()

getNode(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole

Get the body Q Node direction in ICRF frame.

getNode(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole

Get the body Q Node direction in ICRF frame.

getNoise() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Generate a noise vector.

getNominalTidalDisplacement() - Method in enum org.orekit.utils.IERSConventions

Get the nominal values of the displacement numbers.

getNonInterpolatingEOPHistory() - Method in class org.orekit.frames.EOPHistory

Get non-interpolating version of the instance.

getNonInterpolatingProvider() - Method in interface org.orekit.frames.EOPBasedTransformProvider

Get a version of the provider that does not cache tidal corrections.

getNonInterpolatingProvider() - Method in class org.orekit.frames.GTODProvider

Get a version of the provider that does not cache tidal corrections.

getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory

Get the transform between two frames, suppressing all interpolation.

getNonInterpolatingTransform(Frame, Frame, FieldAbsoluteDate<T>) - Static method in class org.orekit.frames.FramesFactory

Get the transform between two frames, suppressing all interpolation.

getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries

Get the number of different terms in the non-polynomial part.

getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for Non-Rotating Origin paradigm.

getNonRotatinOriginNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for Non-Rotating Origin paradigm.

getNoradID() - Method in class org.orekit.files.ccsds.OMMFile

Get the NORAD Catalog Number ("Satellite Number").

getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet

Get unit normal vector.

getNormal(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get solar array normal in spacecraft frame.

getNormal(AbsoluteDate, Frame, Vector3D, Rotation) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get solar array normal in spacecraft frame.

getNormal(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get solar array normal in spacecraft frame.

getNormalGravity(double) - Method in class org.orekit.models.earth.ReferenceEllipsoid

Gets the normal gravity, that is gravity just due to the reference ellipsoid's potential.

getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.

getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the gravity field coefficients provider from the first supported file.

getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a NormalizedSphericalHarmonicsProvider from an UnnormalizedSphericalHarmonicsProvider.

getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics

Get a spherical harmonic sine coefficient.

getNormalizedValue() - Method in class org.orekit.utils.ParameterDriver

Get normalized value.

getNorth() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction to the north of point, expressed in parent shape frame.

getNorth() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction to the north of point, expressed in parent shape frame.

getNorth() - Method in class org.orekit.frames.TopocentricFrame

Get the north direction of topocentric frame, expressed in parent shape frame.

getNorthOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station position along North axis.

getNumber() - Method in interface org.orekit.estimation.measurements.EstimationsProvider

Get the number of evaluations available.

getNumber() - Method in enum org.orekit.time.Month

Get the month number.

getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3File

Returns the number of epochs contained in this orbit file.

getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the fundamental nutation arguments.

getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions

Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.

getNutationFunction() - Method in enum org.orekit.utils.IERSConventions

Get the function computing the nutation angles.

getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions

Get the reference epoch for fundamental nutation arguments.

getObjectID() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the spacecraft ID for which the orbit state is provided.

getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the function computing position/velocity at sample points.

getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter

Get the function computing position/velocity at sample points.

getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter

Get the function computing position/velocity at sample points.

getObjectName() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the spacecraft name for which the orbit state is provided.

getObservationCode() - Method in class org.orekit.gnss.RinexHeader

Get the observation code of the average phasecenter position w/r to antenna reference point.

getObservationData() - Method in class org.orekit.gnss.ObservationDataSet

Get list of observation data.

getObservationDataSets() - Method in class org.orekit.gnss.RinexLoader

Get parsed rinex observations data sets.

getObservations() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Get the list of Observations data lines.

getObservations() - Method in class org.orekit.gnss.RinexLoader

Deprecated.

as of 9.3 replaced by RinexLoader.getObservationDataSets()

getObservationsBlocks() - Method in class org.orekit.files.ccsds.TDMFile

Get the list of observations blocks as an unmodifiable list.

getObservationsComment() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Get the observations data lines comment.

getObservationType() - Method in class org.orekit.gnss.ObservationData

Get the observation type.

getObservedMeasurement() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the associated observed measurement.

getObservedMeasurement() - Method in class org.orekit.estimation.sequential.MeasurementDecorator

Get the observed measurement.

getObservedValue() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the observed value.

getObservedValue() - Method in interface org.orekit.estimation.measurements.ComparableMeasurement

Get the observed value.

getObservedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the observed value.

getObserver() - Method in class org.orekit.propagation.events.AngularSeparationDetector

Get the observer for the spacecraft.

getObserverName() - Method in class org.orekit.gnss.RinexHeader

Get name of the observer.

getObservers() - Method in class org.orekit.utils.ParameterDriver

Get the observers for this driver.

getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector

Get the occulted body.

getOcculted() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Get the occulted body.

getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector

Get the occulted body radius (m).

getOccultedRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Get the occulted body radius (m).

getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector

Get the occulting body.

getOcculting() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Get the occulting body.

getOccultingRadius() - Method in class org.orekit.propagation.events.EclipseDetector

Get the occulting body radius (m).

getOccultingRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Get the occulting body radius (m).

getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the configured ocean load deformation coefficients.

getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions

Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).

getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the ocean tides waves from the first supported file.

getODMFile() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the ODM file to which these meta-data belong.

getOffset() - Method in class org.orekit.time.OffsetModel

Offset at reference date in seconds (TAI minus UTC).

getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the offset from reference date for the harmonics.

getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the offset from reference date for the harmonics.

getOffsetGeodeticPoint() - Method in class org.orekit.estimation.measurements.GroundStation

Deprecated.

as of 9.1, replaced by GroundStation.getOffsetGeodeticPoint(AbsoluteDate)

getOffsetGeodeticPoint(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation

Get the geodetic point at the center of the offset frame.

getOffsetToInertial(Frame, AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation

Get the transform between offset frame and inertial frame.

getOffsetToInertial(Frame, AbsoluteDate, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation

Get the transform between offset frame and inertial frame with derivatives.

getOffsetToInertial(Frame, FieldAbsoluteDate<DerivativeStructure>, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation

Get the transform between offset frame and inertial frame with derivatives.

getOmega() - Method in class org.orekit.data.DelaunayArguments

Get the mean longitude of the ascending node of the Moon.

getOmega() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean longitude of the ascending node of the Moon.

getOmega0() - Method in class org.orekit.gnss.GPSAlmanac

getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.

getOmegaDot() - Method in class org.orekit.data.DelaunayArguments

Get the mean longitude of the ascending node of the Moon time derivative.

getOmegaDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean longitude of the ascending node of the Moon time derivative.

getOmegaDot() - Method in class org.orekit.gnss.GPSAlmanac

getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Rate of Right Ascension.

getOptimum() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the optimum found.

getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState

Gets the current orbit.

getOrbit() - Method in class org.orekit.propagation.SpacecraftState

Gets the current orbit.

getOrbitalParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the drivers for the configurable orbital parameters.

getOrbitalParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the drivers for the configurable orbital parameters.

getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the orbital parameters supported by this estimator.

getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator

Get the orbital parameters supported by this estimator.

getOrbitType() - Method in class org.orekit.files.sp3.SP3File

Returns the SP3File.SP3OrbitType for this SP3 file.

getOrbitType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

getOrbitType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

getOrbitType() - Method in class org.orekit.propagation.events.PositionAngleDetector

Get the orbit type defining the angle type.

getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get propagation parameter type.

getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3File

Returns the orbit type key for this SP3 file.

getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader

Returns a copy of the ordinate grid for the interpolation function.

getOrientation() - Method in class org.orekit.attitudes.Attitude

Get the complete orientation including spin.

getOrientation() - Method in class org.orekit.attitudes.FieldAttitude

Get the complete orientation including spin.

getOrigin() - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Get the origin ITRF.

getOrigin() - Method in class org.orekit.frames.ITRFVersion.Converter

Get the origin ITRF.

getOriginator() - Method in class org.orekit.files.ccsds.ODMFile

Get the file originator.

getOriginator() - Method in class org.orekit.files.ccsds.TDMFile

Get the file originator.

getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the y component of inclination vector.

getPa() - Method in class org.orekit.data.BodiesElements

Get the general accumulated precession in longitude.

getPa() - Method in class org.orekit.data.FieldBodiesElements

Get the general accumulated precession in longitude.

getPa() - Method in class org.orekit.files.ccsds.OGMFile

Get the orbit argument of pericenter.

getPa() - Method in class org.orekit.gnss.GPSAlmanac

getPa() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Argument of Perigee.

getPaDot() - Method in class org.orekit.data.BodiesElements

Get the general accumulated precession in longitude time derivative.

getPaDot() - Method in class org.orekit.data.FieldBodiesElements

Get the general accumulated precession in longitude time derivative.

getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the partial derivatives of the simulated measurement with respect to a parameter.

getParameterDriver(String) - Method in class org.orekit.forces.AbstractForceModel

Get parameter value from its name.

getParameterDriver(String) - Method in interface org.orekit.forces.ForceModel

Get parameter value from its name.

getParameters() - Method in interface org.orekit.forces.ForceModel

Get force model parameters.

getParameters() - Method in interface org.orekit.models.earth.MappingFunction

Get tropospheric model parameters.

getParameters() - Method in class org.orekit.propagation.numerical.JacobiansMapper

Get the number of parameters.

getParameters(Field<T>) - Method in interface org.orekit.forces.ForceModel

Get force model parameters.

getParameters(Field<T>) - Method in interface org.orekit.models.earth.MappingFunction

Get tropospheric model parameters.

getParameters(FieldSpacecraftState<DerivativeStructure>, DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter

Get the tropospheric model parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the drivers for this measurement parameters, including its modifiers parameters.

getParametersDrivers() - Method in interface org.orekit.estimation.measurements.EstimationModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the drivers for this measurement parameters, including its modifiers parameters.

getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce

Get the drivers for force model parameters.

getParametersDrivers() - Method in interface org.orekit.forces.ForceModel

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.NewtonianAttraction

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.OceanTides

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.Relativity

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.SolidTides

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.HarmonicParametricAcceleration

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.PolynomialParametricAcceleration

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the drivers for force model parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.EstimatedTroposphericModel

getParametersDrivers() - Method in class org.orekit.models.earth.GlobalMappingFunctionModel

Get the drivers for tropospheric model parameters.

getParametersDrivers() - Method in interface org.orekit.models.earth.MappingFunction

Get the drivers for tropospheric model parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.MendesPavlisModel

Get the drivers for tropospheric model parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.NiellMappingFunctionModel

getParametersDrivers() - Method in interface org.orekit.models.earth.TroposphericModel

Get the drivers for tropospheric model parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.ViennaOneModel

Get the drivers for tropospheric model parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.ViennaThreeModel

Get the drivers for tropospheric model parameters.

getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper

Get theJacobian with respect to parameters from a one-dimensional additional state array.

getParent() - Method in class org.orekit.frames.Frame

Get the parent frame.

getParentShape() - Method in class org.orekit.frames.TopocentricFrame

Get the body shape on which the local point is defined.

getParticipants() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the coordinates of the measurements participants in signal travel order.

getParticipants() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the participants.

getParts() - Method in interface org.orekit.errors.LocalizedException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitIllegalArgumentException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitIllegalStateException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitInternalError

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitIOException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitParseException

Get the variable parts of the error message.

getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Dummy date at infinity in the past direction.

getPath() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the path.

getPath1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the path1.

getPath2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the path2.

getPdop() - Method in class org.orekit.gnss.DOP

Gets the position dilution of precision.

getPendingEvent() - Method in class org.orekit.propagation.events.FieldEventState

Get PendingEvent.

getPerigeeArgument() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the perigee argument.

getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit

Get the perigee argument.

getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the argument of perigee.

getPerigeeArgumentDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the perigee argument derivative.

getPerigeeArgumentDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the perigee argument derivative.

getPermanentTide() - Method in enum org.orekit.utils.IERSConventions

Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.

getPhase(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide

Get the phase of the tide.

getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern

Get the value of the phase center variation in a signal direction.

getPhaseCenterVariation(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna

Get the value of the phase center variation in a signal direction.

getPhaseShiftCorrections() - Method in class org.orekit.gnss.RinexHeader

Get the list of phase shift correction used to generate phases consistent w/r to cycle shifts.

getPhysicalCovariances(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the covariances matrix in space flight dynamics physical units.

getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanEstimator

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.Model

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the "physical" estimated state (i.e.

getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.KalmanEstimator

Get the "physical" estimated state (i.e.

getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.Model

Get the "physical" estimated state (i.e.

getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the physical innovation covariance matrix.

getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.Model

Get the physical innovation covariance matrix.

getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the physical Kalman gain matrix.

getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.Model

Get the physical Kalman gain matrix.

getPhysicalMeasurementJacobian() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the physical Jacobian of the measurement with respect to the state (H matrix).

getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.Model

Get the physical Jacobian of the measurement with respect to the state (H matrix).

getPhysicalStateTransitionMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get physical state transition matrix between previous state and estimated (but not yet corrected) state.

getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.Model

Get physical state transition matrix between previous state and estimated (but not yet corrected) state.

getPlaneSection(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid

Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.

getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers

Get the real part of a nominal Love numbers.

getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Pluto singleton body.

getPoint() - Method in class org.orekit.frames.TopocentricFrame

Get the surface point defining the origin of the frame.

getPoint(Field<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the surface point defining the origin of the frame.

getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a polar drift along X.

getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a polar drift along X.

getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a polar drift along Y.

getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a polar drift along Y.

getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a polar offset along X.

getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a polar offset along X.

getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a polar offset along Y.

getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a polar offset along Y.

getPolarRadius() - Method in class org.orekit.models.earth.ReferenceEllipsoid

Get the radius of this ellipsoid at the poles.

getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole

Get the body North pole direction in ICRF frame.

getPole(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole

Get the body North pole direction in ICRF frame.

getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the pole IERS Reference Pole correction.

getPoleCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the pole IERS Reference Pole correction.

getPolynomial() - Method in class org.orekit.data.PoissonSeries

Get the polynomial part of the series.

getPosition() - Method in class org.orekit.estimation.measurements.Position

Get the position.

getPosition() - Method in class org.orekit.estimation.measurements.PV

Get the position.

getPosition() - Method in class org.orekit.files.ccsds.OPMFile

Get position vector.

getPosition() - Method in class org.orekit.utils.FieldPVCoordinates

Gets the position.

getPosition() - Method in class org.orekit.utils.PVCoordinates

Gets the position.

getPositionAngle() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the positionAngle.

getPositionAngle() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

getPositionAngle() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

getPositionAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector

Get the type of position angle.

getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get propagation parameter type.

getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the position scale.

getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions

Get the function computing the precession angles.

getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the predicted measurement.

getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.Model

Get the predicted measurement.

getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the predicted spacecraft states.

getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.Model

Get the predicted spacecraft states.

getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Get the local pressure at the evaluation location.

getPressure() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model

Returns the pressure at the station [hPa].

getPressure() - Method in class org.orekit.models.earth.GlobalPressureTemperatureModel

Get the atmospheric pressure of the station depending its position.

getPreviousState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Get the state at previous grid point date.

getPreviousState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the state at previous grid point date.

getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole

Get the prime meridian angle.

getPrimeMeridianAngle(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole

Get the prime meridian angle.

getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a prime meridian rotation rate.

getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a prime meridian rotation rate.

getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a prime meridian rotation.

getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a prime meridian rotation.

getPRN() - Method in class org.orekit.gnss.GPSAlmanac

getPRN() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the PRN number of the GPS satellite.

getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get PRN number.

getPrnNumber() - Method in class org.orekit.gnss.ObservationDataSet

Get PRN number.

getPRNNumbers() - Method in class org.orekit.gnss.SEMParser

Gets the PRN numbers of all the GPS almanacs read from the file.

getPRNNumbers() - Method in class org.orekit.gnss.YUMAParser

Gets the PRN numbers of all the GPS almanacs read from the file.

getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.ConstantProcessNoise

Get the process noise matrix between previous and current states.

getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider

Get the process noise matrix between previous and current states.

getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Get the process noise matrix between previous and current states.

getProgDCBS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS

Get the program name used to apply DCBs.

getProgPCVS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS

Get the program name used to apply PCVs.

getPropagationParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the drivers for the configurable propagation parameters.

getPropagationParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the drivers for the configurable propagation parameters.

getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator

Get the propagator parameters supported by this estimator.

getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the propagationParametersEvolution.

getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

View this ephemeris segment as a propagator.

getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

View this ephemeris as a propagator, combining data from all segments.

getPropagator() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the reference propagator.

getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator

Get a registered propagator.

getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite

Get the index of the propagator related to this satellite.

getPropagatorParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the propagator parameters supported by this estimator.

getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer

Get an unmodifiable list of the underlying mono-satellite propagators.

getPropagatorsIndices() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Deprecated.

as of 9.3, replaced by AbstractMeasurement.getSatellites()

getPropagatorsIndices() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Deprecated.

as of 9.3, replaced by ObservedMeasurement.getSatellites()

getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Get the spherical harmonics provider.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader

Get a provider for read spherical harmonics coefficients.

getProviders() - Method in class org.orekit.data.DataProvidersManager

Get an unmodifiable view of the list of supported providers.

getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationDetector

Get the proximity angle (rad).

getPVCoordinates() - Method in class org.orekit.files.ccsds.OPMFile

Get the position/velocity coordinates contained in the OPM.

getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit

Get the TimeStampedPVCoordinates in definition frame.

getPVCoordinates() - Method in class org.orekit.orbits.Orbit

Get the TimeStampedPVCoordinates in definition frame.

getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the TimeStampedFieldPVCoordinates in orbit definition frame.

getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState

Get the TimeStampedPVCoordinates in orbit definition frame.

getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit

Get the TimeStampedPVCoordinates in a specified frame.

getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit

Get the TimeStampedPVCoordinates in a specified frame.

getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState

Get the TimeStampedFieldPVCoordinates in given output frame.

getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState

Get the TimeStampedPVCoordinates in given output frame.

getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the extrapolated position and velocity from an initial TLE.

getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Get the extrapolated position and velocity from an initial date.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame

Get the PVCoordinates of the topocentric frame origin in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector

Get the body to align.

getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Get PV coordinates provider.

getPvProvider() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Get PV coordinates provider.

getPVTarget() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector

Get the position/velocity provider of the target .

getPVTarget() - Method in class org.orekit.propagation.events.FieldOfViewDetector

Get the position/velocity provider of the target .

getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the x component of inclination vector.

getQZSS() - Static method in class org.orekit.time.TimeScalesFactory

Get the Quasi-Zenith Satellite System time scale.

getRaan() - Method in class org.orekit.files.ccsds.OGMFile

Get the orbit right ascension of ascending node.

getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE

Get Right Ascension of the Ascending node.

getRadiationParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get the drivers for supported parameters.

getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Get the drivers for supported parameters.

getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Get the drivers for supported parameters.

getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Get the drivers for supported parameters.

getRadiationParametersDrivers() - Method in interface org.orekit.forces.radiation.RadiationSensitive

Get the drivers for supported parameters.

getRange(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the range of a point with regards to the topocentric frame center point.

getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the range of a point with regards to the topocentric frame center point.

getRange1() - Method in class org.orekit.estimation.iod.IodGooding

Get the range for observation (1).

getRange2() - Method in class org.orekit.estimation.iod.IodGooding

Get the range for observation (2).

getRange3() - Method in class org.orekit.estimation.iod.IodGooding

Get the range for observation (3).

getRangeMode() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the rangeMode.

getRangeModulus() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the rangeModulus.

getRangeRate(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the range rate of a point with regards to the topocentric frame center point.

getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the range rate of a point with regards to the topocentric frame center point.

getRangeUnits() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the rangeUnits.

getRate(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide

Get the angular rate of the tide.

getRatio() - Method in enum org.orekit.gnss.Frequency

Get the ratio f/f0, where f0 is the common frequency.

getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getRawDrivers() - Method in class org.orekit.utils.ParameterDriversList.DelegatingDriver

Get the raw drivers to which this one delegates.

getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the underlying provider for raw (non-interpolated) transforms.

getRawProvider() - Method in class org.orekit.frames.ShiftingTransformProvider

Get the underlying provider for raw (non-interpolated) transforms.

getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider

Get the position-velocity at date.

getRawPV(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider

Get the position-velocity at date.

getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics

Get a spherical harmonic sine coefficient.

getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get the critical distance.

getRcvrClkOffset() - Method in class org.orekit.gnss.ObservationDataSet

Get receiver clock offset.

getReal(int, int) - Method in class org.orekit.utils.LoveNumbers

Get the real part of a nominal Love numbers.

getReceiveBand() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the receiveBand.

getReceiveDelays() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for receiveDelays.

getReceiverNumber() - Method in class org.orekit.gnss.RinexHeader

Get the number of the receiver.

getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader

Get parsed receivers antennas.

getReceiverType() - Method in class org.orekit.gnss.RinexHeader

Get the type of the receiver.

getReceiverVersion() - Method in class org.orekit.gnss.RinexHeader

Get the version of the receiver.

getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate

Get the reference attitude.

getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the reference date for the harmonics.

getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the reference date for the harmonics.

getReferenceDate() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get reference date.

getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper

Get reference date.

getReferenceDate() - Method in class org.orekit.utils.ParameterDriver

Get current reference date.

getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic

Get the reference date.

getReferenceFrame() - Method in class org.orekit.attitudes.Attitude

Get the reference frame.

getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitude

Get the reference frame.

getReferenceFrame() - Method in class org.orekit.estimation.measurements.AngularRaDec

Get the reference frame in which the right ascension - declination angles are given.

getReferenceFrame() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Get the the value of REFERENCE_FRAME as an Orekit Frame.

getReferenceFrameString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Get the reference frame specifier as it appeared in the file.

getReferenceValue() - Method in class org.orekit.utils.ParameterDriver

Get reference parameter value.

getRefFrame() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame

Get the name of the CCSDS reference frame.

getRefFrame() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the the value of REF_FRAME as an Orekit Frame.

getRefFrame() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get Coordinate system for velocity increment vector, for absolute frames.

getRefLofType() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get coordinate system for velocity increment vector, for Local Orbital Frames.

getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel

Compute the refraction angle from the true (geometrical) elevation.

getRefraction(double) - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction

getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured refraction model.

getRefractionModel() - Method in class org.orekit.propagation.events.FieldElevationDetector

Returns the currently configured refraction model.

getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the retrograde factor.

getRevAtEpoch() - Method in class org.orekit.files.ccsds.OMMFile

Get the revolution rumber.

getReversedProvider(TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils

Reverse a transform provider.

getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the revolution number.

getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit

Get the right ascension of the ascending node.

getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the right ascension of the ascending node.

getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the right ascension of the ascending node.

getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit

Get the right ascension of the ascending node.

getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.CircularOrbit

Get the right ascension of the ascending node derivative.

getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the right ascension of the ascending node derivative.

getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the right ascension of the ascending node derivative.

getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the right ascension of the ascending node derivative.

getRinexVersion() - Method in class org.orekit.gnss.RinexHeader

Get Rinex Version.

getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the Root Mean Square Deviation of the fitting.

getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds

Get the upper bound value R^ε_n,m,l(γ).

getRoot() - Static method in class org.orekit.frames.Frame

Get the unique root frame.

getRotation() - Method in class org.orekit.attitudes.Attitude

Get the attitude rotation.

getRotation() - Method in class org.orekit.attitudes.FieldAttitude

Get the attitude rotation.

getRotation() - Method in class org.orekit.frames.FieldTransform

Get the underlying elementary rotation.

getRotation() - Method in class org.orekit.frames.Transform

Get the underlying elementary rotation.

getRotation() - Method in class org.orekit.utils.AngularCoordinates

Get the rotation.

getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates

Get the rotation.

getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude

Get the satellite rotation acceleration.

getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude

Get the satellite rotation acceleration.

getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform

Get the second time derivative of the rotation.

getRotationAcceleration() - Method in class org.orekit.frames.Transform

Get the second time derivative of the rotation.

getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates

Get the rotation acceleration.

getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates

Get the rotation acceleration.

getRotationRate() - Method in class org.orekit.frames.FieldTransform

Get the first time derivative of the rotation.

getRotationRate() - Method in class org.orekit.frames.Transform

Get the first time derivative of the rotation.

getRotationRate() - Method in class org.orekit.utils.AngularCoordinates

Get the rotation rate.

getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates

Get the rotation rate.

getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

Get s.

getS10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the EUV index (26-34 nm) scaled to F10.

getS10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the EUV 81-day averaged centered index.

getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the states sample.

getSatConfiguration() - Method in class org.orekit.gnss.GPSAlmanac

Gets the satellite configuration.

getSatelliteCode() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get satellite code.

getSatelliteCount() - Method in class org.orekit.files.sp3.SP3File

Get the number of satellites contained in this orbit file.

getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the satellite id.

getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the number of satellite revolutions to use for converting osculating to mean elements.

getSatellites() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the satellites related to this measurement.

getSatellites() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the satellites related to this measurement.

getSatellites() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the satellites related to this measurement.

getSatellites() - Method in class org.orekit.files.ccsds.OEMFile

getSatellites() - Method in interface org.orekit.files.general.EphemerisFile

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in class org.orekit.files.general.OrekitEphemerisFile

getSatellites() - Method in class org.orekit.files.sp3.SP3File

getSatellitesAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader

Get parsed satellites antennas.

getSatelliteSystem() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get satellite system.

getSatelliteSystem() - Method in enum org.orekit.gnss.Frequency

Get the satellite system for which this frequency is defined.

getSatelliteSystem() - Method in class org.orekit.gnss.ObservationDataSet

Get Satellite System.

getSatelliteSystem() - Method in class org.orekit.gnss.RinexHeader

Get Satellite System.

getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS

Get the satellite system.

getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS

Get the satellite system.

getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection

Get the Satellite System.

getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.ScaleFactorCorrection

Get the Satellite System.

getSatelliteType() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get satellite type.

getSatsCorrected() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection

Get the list of satellites involved.

getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Saturn singleton body.

getScale() - Method in class org.orekit.utils.ParameterDriver

Get scale.

getSecond() - Method in class org.orekit.time.TimeComponents

Get the seconds number.

getSecondsInLocalDay() - Method in class org.orekit.time.TimeComponents

Get the second number within the local day, without applying the offset from UTC.

getSecondsInUTCDay() - Method in class org.orekit.time.TimeComponents

Get the second number within the UTC day, applying the offset from UTC.

getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3File

Returns the seconds of the GPS week as contained in the SP3 file.

getSegments() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris

getSegments() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the segments of the ephemeris.

getSegments() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

getSegments() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

Returns a list containing only this.

getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the selected short periodic coefficients that must be stored as additional states.

getSelectedNormalizedParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the current value of selected normalized parameters.

getSelectedNormalizedParameters() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the current value of selected normalized parameters.

getSelectedParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Get the selected parameters, in Jacobian matrix column order.

getSelector() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler

Get the dates selector.

getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna

Get the serial number.

getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter

Get the current value of sigma.

getSignalStrength() - Method in class org.orekit.gnss.ObservationData

Get the signal strength.

getSignalStrengthUnit() - Method in class org.orekit.gnss.RinexHeader

Get the unit of the carrier to noise ratio observables.

getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna

Get the sinex code of the antenna.

getSiteLocation() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the site location.

getSiteName() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the site name.

getSites() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

Get the list of sites for which we have found coefficients, in lexicographic order ignoring case.

getSize() - Method in class org.orekit.utils.LoveNumbers

Get the size of the arrays.

getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the S_j coefficient.

getSlave() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Get the provider for the slave satellite.

getSlaveStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange

Get the slave ground station reflecting the signal.

getSlope() - Method in class org.orekit.time.OffsetModel

Offset slope in seconds per UTC day (TAI minus UTC / dUTC).

getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of slots in use.

getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of slots evictions.

getSma() - Method in class org.orekit.gnss.GPSAlmanac

getSma() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Semi-Major Axis.

getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the semi-major axis.

getSolarRadArea() - Method in class org.orekit.files.ccsds.OGMFile

Get the solar radiation pressure area.

getSolarRadCoeff() - Method in class org.orekit.files.ccsds.OGMFile

Get the solar radiation pressure coefficient.

getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the solar system barycenter aggregated body.

getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions

Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).

getSource() - Method in class org.orekit.gnss.GPSAlmanac

Gets the source of this GPS almanac.

getSourceDCBS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS

Get the source of corrections.

getSourcePCVS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS

Get the source of corrections.

getSourceString() - Method in enum org.orekit.errors.OrekitMessages

getSouth() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction to the south of point, expressed in parent shape frame.

getSouth() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction to the south of point, expressed in parent shape frame.

getSouth() - Method in class org.orekit.frames.TopocentricFrame

Get the south direction of topocentric frame, expressed in parent shape frame.

getSouthAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the amplitude along South axis.

getSouthPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the phase along South axis.

getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get spacecraft shape.

getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Get spacecraft shape.

getSpacecraftComment() - Method in class org.orekit.files.ccsds.OGMFile

Get the comment for spacecraft.

getSpan(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Get the time span containing a specified date.

getSpecifier() - Method in interface org.orekit.errors.LocalizedException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalArgumentException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalStateException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitInternalError

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitIOException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitParseException

Get the localizable specifier of the error message.

getSpin() - Method in class org.orekit.attitudes.Attitude

Get the satellite spin.

getSpin() - Method in class org.orekit.attitudes.FieldAttitude

Get the satellite spin.

getSpin() - Method in class org.orekit.models.earth.ReferenceEllipsoid

Gets the rotation of the ellipsoid about its axis.

getStandardModel() - Static method in class org.orekit.models.earth.SaastamoinenModel

Create a new Saastamoinen model using a standard atmosphere model.

getStandardModel(double, double) - Static method in class org.orekit.models.earth.MariniMurrayModel

Create a new Marini-Murray model using a standard atmosphere model.

getStandardModel(double, double) - Static method in class org.orekit.models.earth.MendesPavlisModel

Create a new Mendes-Pavlis model using a standard atmosphere model.

getStart() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the start of the measurements time span.

getStart() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getStart() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris

getStart() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the start date of this ephemeris segment.

getStart() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

getStart() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getStart() - Method in class org.orekit.time.OffsetModel

Get the date of the offset start.

getStart() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the start of this time span.

getStartDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the start date.

getStartDate() - Method in class org.orekit.frames.EOPHistory

Get the date of the first available Earth Orientation Parameters.

getStartDate() - Method in class org.orekit.propagation.AbstractPropagator

Get the start date.

getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the start date.

getStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get start of total time span covered by ephemerides data and covariance data.

getStartTime() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the startTime.

getStartTimeString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the startTime String.

getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the triggering state.

getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent

Get the triggering state.

getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event

Get the spacecraft's state at the event.

getState(DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter

Get the state with the number of parameters consistent with tropospheric model.

getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.

getStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper

Deprecated.

as of 9.0, replaced with JacobiansMapper.STATE_DIMENSION

getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper

Get the Jacobian with respect to state from a one-dimensional additional state array.

getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the states of the spacecrafts.

getStation() - Method in class org.orekit.estimation.measurements.AngularAzEl

Get the ground station from which measurement is performed.

getStation() - Method in class org.orekit.estimation.measurements.AngularRaDec

Get the ground station from which measurement is performed.

getStation() - Method in class org.orekit.estimation.measurements.Phase

Get the ground station from which measurement is performed.

getStation() - Method in class org.orekit.estimation.measurements.Range

Get the ground station from which measurement is performed.

getStation() - Method in class org.orekit.estimation.measurements.RangeRate

Get the ground station from which measurement is performed.

getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the status.

getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the grid points time step.

getStep() - Method in class org.orekit.frames.ShiftingTransformProvider

Get the grid points time step.

getStepHandler() - Method in class org.orekit.propagation.AbstractPropagator

Get the step handler.

getStepHandler() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the step handler.

getStop() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getStop() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris

getStop() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the end date of this ephemeris segment.

getStop() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

getStop() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getStopDate() - Method in class org.orekit.propagation.events.EventState.EventOccurrence

Get the new time for a stop action.

getStopDate() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence

Get the new time for a stop action.

getStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get end of total time span covered by ephemerides data and covariance data.

getStopTime() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the stopTime.

getStopTimeString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the stopTime String.

getStreamOpener() - Method in class org.orekit.data.NamedData

Get the data stream opener.

getStrengthLevel() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the strength level for activity.

getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Sun singleton body.

getSupportedNames() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the supported names for data files.

getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Get the regular expression for supported files names.

getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the regular expression for supported files names.

getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the regular expression for supported files names.

getSupportedNames() - Method in class org.orekit.gnss.SEMParser

Get the supported names for data files.

getSupportedNames() - Method in class org.orekit.gnss.YUMAParser

Get the supported names for data files.

getSupportedNames() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Returns the supported names of the loader.

getSupportedNames() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader

Returns the supported names of the loader.

getSVN() - Method in class org.orekit.gnss.GPSAlmanac

Gets the satellite "SVN" reference number.

getTabDensity() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester

Get the current density table.

getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset

Get an unmodifiable view of the tabulated attitudes.

getTAI() - Static method in class org.orekit.time.TimeScalesFactory

Get the International Atomic Time scale.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the target point position/velocity in specified frame.

getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the size of the target.

getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide

Get the multiplier for the τ Doodson argument.

getTC() - Method in class org.orekit.data.DelaunayArguments

Get the offset in Julian centuries.

getTC() - Method in class org.orekit.data.FieldDelaunayArguments

Get the offset in Julian centuries.

getTCB() - Static method in class org.orekit.time.TimeScalesFactory

Get the Barycentric Coordinate Time scale.

getTCG() - Static method in class org.orekit.time.TimeScalesFactory

Get the Geocentric Coordinate Time scale.

getTDB() - Static method in class org.orekit.time.TimeScalesFactory

Get the Barycentric Dynamic Time scale.

getTdop() - Method in class org.orekit.gnss.DOP

Gets the time dilution of precision.

getTEME() - Static method in class org.orekit.frames.FramesFactory

Get the TEME reference frame.

getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Get the local temperature at the evaluation location.

getTemperature() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model

Returns the temperature at the station [K].

getTemperature() - Method in class org.orekit.models.earth.GlobalPressureTemperatureModel

Get the atmospheric temperature of the station depending its position.

getTFirstObs() - Method in class org.orekit.gnss.RinexHeader

Get the time of First observation record.

getTGD() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the estimated group delay differential TGD for L1-L2 correction.

getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the theoretical standard deviation.

getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the theoretical standard deviation.

getTheoreticalStandardDeviation() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the theoretical standard deviation.

getTheta0() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction

Get the station elevation angle under free-space propagation .

getThetaMin() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction

Get the station minimal elevation angle.

getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the 3 hours geomagnetic index.

getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters

Get the value of the 3 hours geomagnetic index.

getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in class org.orekit.propagation.events.AdapterDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in interface org.orekit.propagation.events.EventDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in interface org.orekit.propagation.events.FieldEventDetector

Get the convergence threshold in the event time search.

getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the thrust.

getTidalDisplacementFrequencyCorrectionDiurnal() - Method in enum org.orekit.utils.IERSConventions

Get the correction function for tidal displacement for diurnal tides.

getTidalDisplacementFrequencyCorrectionDiurnal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions

Get the correction function for tidal displacement for diurnal tides.

getTidalDisplacementFrequencyCorrectionZonal() - Method in enum org.orekit.utils.IERSConventions

Get the correction function for tidal displacement for zonal tides.

getTidalDisplacementFrequencyCorrectionZonal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions

Get the correction function for tidal displacement for zonal tides.

getTide(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the tide.

getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).

getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the TideSystem used in the gravity field.

getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the TideSystem used in the gravity field.

getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the TideSystem used in the gravity field.

getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider

Get the TideSystem used in the gravity field.

getTime() - Method in class org.orekit.estimation.sequential.MeasurementDecorator

getTime() - Method in class org.orekit.gnss.GPSAlmanac

getTime() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Reference Time of the GPS orbit as a duration from week start.

getTime() - Method in class org.orekit.time.DateTimeComponents

Get the time component.

getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the time offset from first state date to measurement date.

getTimeScale() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getTimeScale() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the time scale for this ephemeris segment.

getTimeScale() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getTimeScale() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getTimeScale(IERSConventions) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale

Get the corresponding TimeScale.

getTimeScaleString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

getTimeScaleString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the time scale for this ephemeris segment.

getTimeScaleString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

getTimeScaleString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris

getTimeSystem() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.

getTimeSystem() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.

getTimeSystem() - Method in class org.orekit.files.sp3.SP3File

Returns the SP3File.TimeSystem used to time-stamp position entries.

getTimetagRef() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the timetagRef.

getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory

Get the TIRF reference frame, ignoring tidal effects.

getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the TIRF reference frame.

getTLastObs() - Method in class org.orekit.gnss.RinexHeader

Get the time of last observation record.

getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the underlying TLE.

getTLERelatedParametersComment() - Method in class org.orekit.files.ccsds.OMMFile

Get the comment for TLE related parameters.

getToc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the clock correction reference time toc.

getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory

Get the TOD reference frame.

getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the TOD reference frame.

getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured topocentric frame definitions.

getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationExtremumDetector

Returns the topocentric frame centered on ground point.

getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationDetector

Returns the currently configured topocentric frame definitions.

getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector

Get the total eclipse detection flag.

getTotalEclipse() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Get the total eclipse detection flag.

getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the total intensity of the magnetic field (= norm of the field vector).

getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider

getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<DerivativeStructure>, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get the transform with derivatives.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider

Get the FieldTransform corresponding to specified date.

getTransformation() - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Get the underlying HelmertTransformation.

getTransformProvider() - Method in class org.orekit.frames.Frame

Get the provider for transform from parent frame to instance.

getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame

Get the transform from the instance to another frame.

getTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame

Get the transform from the instance to another frame.

getTransitions() - Method in class org.orekit.utils.FieldTimeSpanMap

Get an unmodifiable view of the sorted transitions.

getTransitions() - Method in class org.orekit.utils.TimeSpanMap

Get an unmodifiable view of the sorted transitions.

getTranslation() - Method in class org.orekit.frames.FieldTransform

Get the underlying elementary translation.

getTranslation() - Method in class org.orekit.frames.Transform

Get the underlying elementary translation.

getTransmitBand() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the transmitBand.

getTransmitDelays() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the transmitDelays.

getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the triggering event.

getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType

Get the increasing status of triggered events.

getTrueAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the true anomaly.

getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit

Get the true anomaly.

getTrueAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the true anomaly derivative.

getTrueAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the true anomaly derivative.

getTT() - Static method in class org.orekit.time.TimeScalesFactory

Get the Terrestrial Time scale.

getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the turnaroundDenominator.

getTurnaroundNumerator() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Getter for the turnaroundNumerator.

getType() - Method in class org.orekit.files.sp3.SP3File

Returns the SP3File.SP3FileType associated with this SP3 file.

getType() - Method in class org.orekit.gnss.antenna.Antenna

Get the type of the antenna.

getType() - Method in class org.orekit.orbits.CartesianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.CircularOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.KeplerianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.Orbit

Get the orbit type.

getTypeObs() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection

Get the Carrier Phase Observation Code.

getTypesObsScaled() - Method in class org.orekit.gnss.RinexLoader.Parser.ScaleFactorCorrection

Get the list of Observation Types scaled.

getU() - Method in class org.orekit.bodies.Ellipse

Get the unit vector along the major axis.

getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier

Get the underlying attitude provider.

getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized

Get the underlying attitude provider.

getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawCompensation

Get the underlying (ground pointing) attitude provider.

getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawSteering

Get the underlying (ground pointing) attitude provider.

getUndulation(double, double, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid

Gets the Undulation of the Geoid, N at the given position.

getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get a un-normalization factors array.

getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.

getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the gravity field coefficients provider from the first supported file.

getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create an UnnormalizedSphericalHarmonicsProvider from a NormalizedSphericalHarmonicsProvider.

getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics

Get a spherical harmonic sine coefficient.

getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month

Get the upper case three letters abbreviation.

getUpperCaseName() - Method in enum org.orekit.time.Month

Get the upper case full name.

getURA() - Method in class org.orekit.gnss.GPSAlmanac

Gets the average URA number.

getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Uranus singleton body.

getUseableStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

getUseableStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

getUserDefinedParameters() - Method in class org.orekit.files.ccsds.OGMFile

Get the map of user defined parameter keywords and their corresponding values.

getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time 1 scale.

getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time 1 scale.

getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry

Get the UT1-UTC value.

getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the UT1-UTC value.

getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the UT1-UTC value.

getUTC() - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time Coordinate scale.

getUTCScale() - Method in class org.orekit.time.UT1Scale

Get the associated UTC scale.

getV() - Method in class org.orekit.bodies.Ellipse

Get the unit vector along the minor axis.

getValidFrom() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get start of validity.

getValidFUntil() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get end of validity.

getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator

getValue() - Method in class org.orekit.gnss.ObservationData

Get the observed value.

getValue() - Method in class org.orekit.utils.ParameterDriver

Get current parameter value.

getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the value of the Hansen coefficient K_j^{-n-1, s}.

getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Compute the value of the Hansen coefficient K₀^{n, s}.

getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Get the K₀^-n-1,s coefficient value.

getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Get Γ function value.

getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators

Get the Newcomb operator evaluated at n, s, ρ, σ.

getValue(int, int, int, DerivativeStructure) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials

Returns the value and derivatives of the Jacobi polynomial P_l^v,w evaluated at γ.

getValue(DSFactory, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver

Get the value as a derivative structure.

getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader

Returns a copy of the values samples for the interpolation function.

getVdop() - Method in class org.orekit.gnss.DOP

Gets the vertical dilution of precision.

getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get equinoctial frame vector f.

getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get equinoctial frame vector g.

getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get equinoctial frame vector w.

getVeis1950() - Static method in class org.orekit.frames.FramesFactory

Get the VEIS 1950 reference frame.

getVelocity() - Method in class org.orekit.estimation.measurements.PV

Get the velocity.

getVelocity() - Method in class org.orekit.files.ccsds.OPMFile

Get velocity vector.

getVelocity() - Method in class org.orekit.frames.FieldTransform

Get the first time derivative of the translation.

getVelocity() - Method in class org.orekit.frames.Transform

Get the first time derivative of the translation.

getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates

Gets the velocity.

getVelocity() - Method in class org.orekit.utils.PVCoordinates

Gets the velocity.

getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere

Get the inertial velocity of atmosphere molecules.

getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere

Get the inertial velocity of atmosphere molecules.

getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Venus singleton body.

getVertices() - Method in class org.orekit.models.earth.tessellation.Tile

Get the four vertices.

getVmns(int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Get the V_n,s^m coefficient from V_n,s.

getWarmup() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter

Get the value of warmup iterations.

getWaterVaporPressure() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model

Returns the water vapor pressure at the station [hPa].

getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the loaded waves.

getWeek() - Method in class org.orekit.gnss.GPSAlmanac

getWeek() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Gets the Reference Week of the GPS orbit.

getWeekNumber() - Method in class org.orekit.time.GPSDate

Get the week number since GPS epoch.

getWest() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction to the west of point, expressed in parent shape frame.

getWest() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction to the west of point, expressed in parent shape frame.

getWest() - Method in class org.orekit.frames.TopocentricFrame

Get the west direction of topocentric frame, expressed in parent shape frame.

getWestAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the amplitude along west axis.

getWestPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the phase along West axis.

getWgs84(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid

Get the WGS84 ellipsoid, attached to the given body frame.

getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory

Get the WMM model for the given year.

getX() - Method in class org.orekit.frames.EOPEntry

Get the X component of the pole motion.

getXM10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the MG2 index scaled to F10.

getXM10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the MG2 81-day average centered index.

getXp() - Method in class org.orekit.frames.FieldPoleCorrection

Get the x_p parameter.

getXp() - Method in class org.orekit.frames.PoleCorrection

Get the x_p parameter.

getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions

Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.

getY() - Method in class org.orekit.frames.EOPEntry

Get the Y component of the pole motion.

getY10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the Solar X-Ray & Lya index scaled to F10.

getY10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters

Get the Solar X-Ray & Lya 81-day ave.

getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the yaw compensation angle at date.

getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the yaw compensation angle at date.

getYear() - Method in enum org.orekit.frames.ITRFVersion

Get the reference year of the frame version.

getYear() - Method in class org.orekit.time.DateComponents

Get the year number.

getYp() - Method in class org.orekit.frames.FieldPoleCorrection

Get the y_p parameter.

getYp() - Method in class org.orekit.frames.PoleCorrection

Get the y_p parameter.

getZenith() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction above the point, expressed in parent shape frame.

getZenith() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction above the point, expressed in parent shape frame.

getZenith() - Method in class org.orekit.frames.TopocentricFrame

Get the zenith direction of topocentric frame, expressed in parent shape frame.

getZenithAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the amplitude along zenith axis.

getZenithDelay() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader

Returns the zenith delay array.

getZenithOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station position along Zenith axis.

getZenithPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the phase along zenith axis.

getZero(Field<T>) - Static method in class org.orekit.utils.FieldPVCoordinates

Get fixed position/velocity at origin (both p, v and a are zero vectors).

getZone() - Method in class org.orekit.propagation.events.FieldOfView

Get the interior zone.

getZone() - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Get the geographic zone triggering the events.

getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector

Get the geographic zone.

GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the G_js, H_js, I_js and J_js polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.

GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Create a set of G_js, H_js, I_js and J_js polynomials.

GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the G_ms^j and the H_ms^j polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.

GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Create a set of G_ms^j and H_ms^j polynomials.

GillIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for GillIntegrator.

GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder

Build a new instance.

GLO - org.orekit.files.sp3.SP3File.TimeSystem

GLONASS.

GlobalMappingFunctionModel - Class in org.orekit.models.earth

The Global Mapping Function model for radio techniques.

GlobalMappingFunctionModel(double, double) - Constructor for class org.orekit.models.earth.GlobalMappingFunctionModel

Build a new instance.

GlobalPressureTemperature2Model - Class in org.orekit.models.earth

The Global Pressure and Temperature 2 (GPT2) model.

GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.GlobalPressureTemperature2Model

Constructor with default supported names.

GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.GlobalPressureTemperature2Model

Constructor with supported names given by user.

GlobalPressureTemperatureModel - Class in org.orekit.models.earth

The Global Pressure and Temperature model.

GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.GlobalPressureTemperatureModel

Build a new instance.

Glonass - Class in org.orekit.gnss.attitude

Attitude providers for Glonass navigation satellites.

Glonass(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Glonass

Simple constructor.

GLONASS - org.orekit.files.sp3.SP3File.SP3FileType

GLONASS only file.

GLONASS - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GLONASS : GLONASS no.

GLONASS - org.orekit.gnss.antenna.SatelliteType

GLONASS : GLONASS no.

GLONASS - org.orekit.gnss.SatelliteSystem

GLONASS system.

GLONASS_K1 - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GLONASS-K1 : IGS SVN R801-R802 (GLO no.

GLONASS_K1 - org.orekit.gnss.antenna.SatelliteType

GLONASS-K1 : IGS SVN R801-R802 (GLO no.

GLONASS_K2 - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GLONASS-K2.

GLONASS_K2 - org.orekit.gnss.antenna.SatelliteType

GLONASS-K2.

GLONASS_M - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

GLONASS-M : GLONASS no.

GLONASS_M - org.orekit.gnss.antenna.SatelliteType

GLONASS-M : GLONASS no.

GLONASSScale - Class in org.orekit.time

GLONASS time scale.

GM - org.orekit.files.ccsds.Keyword

Gravitational coefficient.

GMST - org.orekit.files.ccsds.CcsdsTimeScale

Greenwich Mean Sidereal Time.

GMSTScale - Class in org.orekit.time

Greenwich Mean Sidereal Time.

GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude

Attitude providers for navigation satellites.

GPS - org.orekit.files.ccsds.CcsdsTimeScale

Global Positioning System.

GPS - org.orekit.files.sp3.SP3File.SP3FileType

GPS only file.

GPS - org.orekit.files.sp3.SP3File.TimeSystem

Global Positioning System.

GPS - org.orekit.gnss.SatelliteSystem

GPS system.

GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.

GPS_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for GPS weeks: 1980-01-06.

GPS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

WGS 84 value of the Earth's universal gravitational parameter for GPS user in m³/s².

GPS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Value of Pi for conversion from semicircles to radian.

GPS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Duration of the GPS week in seconds.

GPS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements

Number of weeks in the GPS cycle.

GPSAlmanac - Class in org.orekit.gnss

This class holds a GPS almanac as read from SEM or YUMA files.

GPSAlmanac(String, int, int, int, double, double, double, double, double, double, double, double, double, double, int, int, int) - Constructor for class org.orekit.gnss.GPSAlmanac

Constructor.

GPSBlockIIA - Class in org.orekit.gnss.attitude

Attitude providers for GPS block IIR navigation satellites.

GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA

Simple constructor.

GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA

Deprecated.

as of 9.3 replaced by GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame)

GPSBlockIIF - Class in org.orekit.gnss.attitude

Attitude providers for GPS block IIF navigation satellites.

GPSBlockIIF(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIF

Simple constructor.

GPSBlockIIR - Class in org.orekit.gnss.attitude

Attitude providers for GPS block IIF navigation satellites.

GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR

Simple constructor.

GPSDate - Class in org.orekit.time

Container for date in GPS form.

GPSDate(int, double) - Constructor for class org.orekit.time.GPSDate

Build an instance corresponding to a GPS date.

GPSDate(AbsoluteDate) - Constructor for class org.orekit.time.GPSDate

Build an instance from an absolute date.

GPSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss

This interface provides the minimal set of orbital elements needed by the GPSPropagator.

GPSPropagator - Class in org.orekit.propagation.analytical.gnss

This class aims at propagating a GPS orbit from GPSOrbitalElements.

GPSPropagator.Builder - Class in org.orekit.propagation.analytical.gnss

This nested class aims at building a GPSPropagator.

GPSScale - Class in org.orekit.time

GPS time scale.

gradient(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the gradient of the non-central part of the gravity field.

gradient(FieldAbsoluteDate<T>, FieldVector3D<T>, T) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the gradient of the non-central part of the gravity field.

GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for GraggBulirschStoerIntegrator.

GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder

Build a new instance.

GRAVITY_FIELD_NORMALIZATION_UNDERFLOW - org.orekit.errors.OrekitMessages

GravityFieldFactory - Class in org.orekit.forces.gravity.potential

Factory used to read gravity field files in several supported formats.

GRC - org.orekit.files.ccsds.CCSDSFrame

Greenwich Rotating Coordinates.

GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for GRGS files.

GRGSFormatReader - Class in org.orekit.forces.gravity.potential

Reader for the GRGS gravity field format.

GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader

Simple constructor.

GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.

GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.

GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.

GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.

GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.

GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.

GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from GRIM5C1 model: 6378136.46 m.

GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from GRIM5C1 model: 1.0 / 298.25765.

GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².

GroundAtNightDetector - Class in org.orekit.propagation.events

Detector for ground location being at night.

GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector

Simple constructor.

GroundFieldOfViewDetector - Class in org.orekit.propagation.events

Finder for satellite entry/exit events with respect to a sensor Field Of View attached to an arbitrary frame.

GroundFieldOfViewDetector(Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector

Build a new instance.

GroundPointing - Class in org.orekit.attitudes

Base class for ground pointing attitude providers.

GroundPointing(Frame, Frame) - Constructor for class org.orekit.attitudes.GroundPointing

Default constructor.

GroundStation - Class in org.orekit.estimation.measurements

Class modeling a ground station that can perform some measurements.

GroundStation(TopocentricFrame) - Constructor for class org.orekit.estimation.measurements.GroundStation

Build a ground station ignoring station displacements.

GroundStation(TopocentricFrame, EOPHistory, StationDisplacement...) - Constructor for class org.orekit.estimation.measurements.GroundStation

Simple constructor.

GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.

GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.

GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from GRS80 model: 6378137.0 m.

GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from GRS80 model: 1.0 / 298.257222101.

GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².

GTOD_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined

GTOD, IERS 1996 conventions, with accurate EOP interpolation.

GTOD_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined

GTOD, IERS 1996 conventions, with simple EOP interpolation.

GTOD_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined

GTOD, IERS 2003 conventions, with accurate EOP interpolation.

GTOD_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined

GTOD, IERS 2003 conventions, with simple EOP interpolation.

GTOD_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined

GTOD, IERS 2010 conventions, with accurate EOP interpolation.

GTOD_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined

GTOD, IERS 2010 conventions, with simple EOP interpolation.

GTOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined

GTOD, IERS 1996 conventions without EOP corrections.

GTODProvider - Class in org.orekit.frames

Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).

GTODProvider(IERSConventions, EOPHistory) - Constructor for class org.orekit.frames.GTODProvider

Simple constructor.

GZIP_FILE_PATTERN - Static variable in interface org.orekit.data.DataProvider

Deprecated.

as of 9.2, replaced with GzipFilter

GzipFilter - Class in org.orekit.data

Filter for gzip compressed data.

GzipFilter() - Constructor for class org.orekit.data.GzipFilter

H

h - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

e_y.

H00 - Static variable in class org.orekit.time.TimeComponents

Constant for commonly used hour 00:00:00.

H12 - Static variable in class org.orekit.time.TimeComponents

Constant for commonly used hour 12:00:00.

handleStep(List<OrekitStepInterpolator>, boolean) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler

Handle the current step.

handleStep(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler

Handle the current step.

handleStep(FieldOrekitStepInterpolator<T>, boolean) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler

Handle the current step.

handleStep(FieldOrekitStepInterpolator<T>, boolean) - Method in class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer

Handle the current step.

handleStep(FieldOrekitStepInterpolator<T>, boolean) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Handle the last accepted step.

handleStep(OrekitStepInterpolator, boolean) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler

Handle the current step.

handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer

Handle the current step.

handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Handle the last accepted step.

handleStep(SpacecraftState, boolean) - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment

handleStep(SpacecraftState, boolean) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler

Handle the current step.

HansenTesseralLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t!=0 and n < 0.

HansenTesseralLinear(int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Constructor.

HansenThirdBodyLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t=0 and n > 0.

HansenThirdBodyLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Constructor.

HansenUtilities - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Utilities class.

HansenZonalLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t=0 and n < 0.

HansenZonalLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Constructor.

HarmonicParametricAcceleration - Class in org.orekit.forces

This class implements a parametric acceleration with harmonic signed amplitude.

HarmonicParametricAcceleration(Vector3D, boolean, String, AbsoluteDate, double, int) - Constructor for class org.orekit.forces.HarmonicParametricAcceleration

Simple constructor.

HarmonicParametricAcceleration(Vector3D, AttitudeProvider, String, AbsoluteDate, double, int) - Constructor for class org.orekit.forces.HarmonicParametricAcceleration

Simple constructor.

HarrisPriester - Class in org.orekit.forces.drag.atmosphere

This atmosphere model is the realization of the Modified Harris-Priester model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.forces.drag.atmosphere.HarrisPriester

Simple constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.forces.drag.atmosphere.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.forces.drag.atmosphere.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.forces.drag.atmosphere.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

hasAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState

Check if an additional state is available.

hasAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState

Check if an additional state is available.

hasCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile

Check whether the OPM contains covariance matrix data.

hasDataFor(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Check if the cache has data for the given date using EOPHistory.getStartDate() and EOPHistory.getEndDate().

hasDerivatives() - Method in class org.orekit.orbits.CartesianOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldCartesianOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldCircularOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.Orbit

Check if orbit includes derivatives.

hashCode() - Method in class org.orekit.bodies.FieldGeodeticPoint

hashCode() - Method in class org.orekit.bodies.GeodeticPoint

hashCode() - Method in class org.orekit.models.earth.displacement.Tide

hashCode() - Method in class org.orekit.propagation.analytical.tle.TLE

Get a hashcode for this tle.

hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

hashCode() - Method in class org.orekit.time.AbsoluteDate

Get a hashcode for this date.

hashCode() - Method in class org.orekit.time.DateComponents

hashCode() - Method in class org.orekit.time.DateTimeComponents

hashCode() - Method in class org.orekit.time.FieldAbsoluteDate

Get a hashcode for this date.

hashCode() - Method in class org.orekit.time.TimeComponents

hasKeplerianElements() - Method in class org.orekit.files.ccsds.OGMFile

Check whether the OPM contains Keplerian elements data.

hasNonKeplerianAcceleration(FieldPVCoordinates<T>, double) - Static method in class org.orekit.orbits.FieldOrbit

Check if Cartesian coordinates include non-Keplerian acceleration.

hasNonKeplerianAcceleration(PVCoordinates, double) - Static method in class org.orekit.orbits.Orbit

Check if Cartesian coordinates include non-Keplerian acceleration.

header - org.orekit.files.ccsds.Keyword

Header keyword.

HELIUM - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000

Identifier for helium.

HelmertTransformation - Class in org.orekit.frames

Transformation class for geodetic systems.

HelmertTransformation(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.HelmertTransformation

Build a transform from its primitive operations.

HelmertTransformation.Predefined - Enum in org.orekit.frames

Enumerate for predefined Helmert transformations.

HERMITE - org.orekit.files.ccsds.OEMWriter.InterpolationMethod

Hermite interpolation.

HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for HighamHall54Integrator.

HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder

Build a new instance.

HLM - org.orekit.files.sp3.SP3File.SP3OrbitType

fitted after applying a Helmert transformation.

HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity

This class represents the gravitational field of a celestial body.

HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Creates a new instance.

HYDROGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000

Identifier for hydrogen.

HYPERBOLIC_ORBIT_NOT_HANDLED_AS - org.orekit.errors.OrekitMessages

hyperbolicEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit

Computes the mean anomaly from the hyperbolic eccentric anomaly.

hyperbolicEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Computes the mean anomaly from the hyperbolic eccentric anomaly.

hyperbolicEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit

Computes the true anomaly from the hyperbolic eccentric anomaly.

hyperbolicEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Computes the true anomaly from the hyperbolic eccentric anomaly.

hyperbolicKeplerianToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Deprecated.

as of 9.3 replaced with FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) and FieldOrbit.getPVCoordinates()

I

i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final inclination.

I05 - org.orekit.gnss.Frequency

IRNSS L5.

I09 - org.orekit.gnss.Frequency

IRNSS S (2492.028 MHz).

IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants

Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.

IAU_2015_NOMINAL_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius as defined by IAU 2015 resolution B3: 6.3781e6 (m).

IAU_2015_NOMINAL_EARTH_GM - Static variable in interface org.orekit.utils.Constants

Earth attraction coefficient as defined by IAU 2015 resolution B3: 3.986004e14 (m³/s²).

IAU_2015_NOMINAL_EARTH_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth polar radius as defined by IAU 2015 resolution B3: 6.3568e6 (m).

IAU_2015_NOMINAL_JUPITER_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Jupiter equatorial radius as defined by IAU 2015 resolution B3: 7.1492e7 (m).

IAU_2015_NOMINAL_JUPITER_GM - Static variable in interface org.orekit.utils.Constants

Jupiter attraction coefficient as defined by IAU 2015 resolution B3: 1.2668653e17 (m³/s²).

IAU_2015_NOMINAL_JUPITER_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants

Jupiter polar radius as defined by IAU 2015 resolution B3: 6.6854e7 (m).

IAU_2015_NOMINAL_SOLAR_RADIUS - Static variable in interface org.orekit.utils.Constants

Solar radius as defined by IAU 2015 resolution B3: 695700000.0 m.

IAU_2015_NOMINAL_SUN_GM - Static variable in interface org.orekit.utils.Constants

Sun attraction coefficient as defined by IAU 2015 resolution B3: 1.3271244e20 (m³/s²).

IAUPole - Interface in org.orekit.bodies

Interface for IAU pole and prime meridian orientations.

ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for ICGEM files.

ICGEMFormatReader - Class in org.orekit.forces.gravity.potential

Reader for the ICGEM gravity field format.

ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader

Simple constructor.

ICRF - org.orekit.files.ccsds.CCSDSFrame

International Celestial Reference Frame.

ICRF - org.orekit.frames.Predefined

ICRF frame.

IDENTITY - Static variable in class org.orekit.frames.Transform

Identity transform.

IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates

Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).

IDENTITY_PROVIDER - Static variable in class org.orekit.frames.TransformProviderUtils

Identity provider.

IERS_1996 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Coefficients from IERS 1996 conventions.

IERS_1996 - org.orekit.utils.IERSConventions

Constant for IERS 1996 conventions.

IERS_2003 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Coefficients from IERS 2003 conventions.

IERS_2003 - org.orekit.utils.IERSConventions

Constant for IERS 2003 conventions.

IERS_2010 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Coefficients from IERS 2010 conventions.

IERS_2010 - org.orekit.utils.IERSConventions

Constant for IERS 2010 conventions.

IERSConventions - Enum in org.orekit.utils

Supported IERS conventions.

IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils

Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.

IGRF - org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel

International Geomagnetic Reference Field.

ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils

A cache of TimeStamped data that provides concurrency through immutability.

ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache

Create a new cache with the given neighbors size and data.

ImpulseManeuver<T extends EventDetector> - Class in org.orekit.forces.maneuvers

Impulse maneuver model.

ImpulseManeuver(T, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

ImpulseManeuver(T, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

INCLINATION - org.orekit.files.ccsds.Keyword

Orbit inclination.

INCOMPLETE_HEADER - org.orekit.errors.OrekitMessages

INCONSISTENT_ASTRONOMICAL_UNIT_IN_FILES - org.orekit.errors.OrekitMessages

INCONSISTENT_DATES_IN_IERS_FILE - org.orekit.errors.OrekitMessages

INCONSISTENT_EARTH_MOON_RATIO_IN_FILES - org.orekit.errors.OrekitMessages

INCONSISTENT_NUMBER_OF_SATS - org.orekit.errors.OrekitMessages

INCONSISTENT_SATELLITE_SYSTEM - org.orekit.errors.OrekitMessages

InertialProvider - Class in org.orekit.attitudes

This class handles an inertial attitude provider.

InertialProvider(Rotation) - Constructor for class org.orekit.attitudes.InertialProvider

Creates new instance.

init(List<SpacecraftState>, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler

Initialize step handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventState

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations

Initialize the equations at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations

Initialize the equations at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler

Initialize step handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer

Initialize step handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Initialize step handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, T) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.ForceModel

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.HarmonicParametricAcceleration

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.PolynomialParametricAcceleration

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AdapterDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.BooleanDetector

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventSlopeFilter

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.handlers.EventHandler

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.NegateDetector

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.PositionAngleDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations

Initialize the equations at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AdditionalEquations

Initialize the equations at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler

Deprecated.

as of 9.0, replaced by OrekitFixedStepHandler.init(SpacecraftState, AbsoluteDate, double)

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate, double) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler

Initialize step handler at the start of a propagation.

init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Initialize builder at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler

Initialize scheduler at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Initialize builder at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.Scheduler

Initialize scheduler at the start of a measurements generation.

INITIAL_MATRIX_AND_PARAMETERS_NUMBER_MISMATCH - org.orekit.errors.OrekitMessages

INITIAL_STATE_NOT_SPECIFIED_FOR_ORBIT_PROPAGATION - org.orekit.errors.OrekitMessages

initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Check if the initial state is provided in osculating elements.

initialize(boolean, AbsoluteDate) - Method in interface org.orekit.propagation.integration.ModeHandler

Initialize the mode handler.

initialize(boolean, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldModeHandler

Initialize the mode handler.

initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Performs initialization prior to propagation for the current force model.

initialize(AuxiliaryElements, boolean) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Performs initialization prior to propagation for the current force model.

initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Performs initialization prior to propagation for the current force model.

initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.

initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Performs initialization prior to propagation for the current force model.

initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Performs initialization at each integration step for the current force model.

initializeStep(AuxiliaryElements) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Performs initialization at each integration step for the current force model.

initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Performs initialization at each integration step for the current force model.

initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Performs initialization at each integration step for the current force model.

initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Performs initialization at each integration step for the current force model.

initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Initialize the mapper.

initMapper() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Initialize the mapper.

initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldCartesianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.Orbit

Compute the position/velocity coordinates from the canonical parameters.

insideLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale

Check if date is within a leap second introduction in this time scale.

insideLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Check if date is within a leap second introduction in this time scale.

insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Check if date is within a leap second introduction in this time scale.

insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale

Check if date is within a leap second introduction in this time scale.

insideLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale

Check if date is within a leap second introduction in this time scale.

insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale

Check if date is within a leap second introduction in this time scale.

IntegratedEphemeris - Class in org.orekit.propagation.integration

This class stores sequentially generated orbital parameters for later retrieval.

IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, boolean, DenseOutputModel, Map<String, double[]>, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris

Creates a new instance of IntegratedEphemeris.

INTEGRATION_INTERVAL - org.orekit.files.ccsds.Keyword

Meta-data: Integration interval.

INTEGRATION_REF - org.orekit.files.ccsds.Keyword

Meta-data: Integration reference.

INTERMEDIATE_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation

Suffix for ground station intermediate frame name.

INTERNAL_ERROR - org.orekit.errors.OrekitMessages

interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolable

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<Attitude>) - Method in class org.orekit.attitudes.Attitude

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<Transform>) - Method in class org.orekit.frames.Transform

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.CartesianOrbit

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.CircularOrbit

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.EquinoctialOrbit

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.KeplerianOrbit

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftState

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.TimeInterpolable

Get an interpolated instance.

interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedAngularCoordinates>) - Static method in class org.orekit.utils.TimeStampedAngularCoordinates

Interpolate angular coordinates.

interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Interpolate angular coordinates.

interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection<TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates

Interpolate position-velocity.

interpolate(AbsoluteDate, CartesianDerivativesFilter, Stream<TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates

Interpolate position-velocity.

interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform

Interpolate a transform from a sample set of existing transforms.

interpolate(FieldAbsoluteDate<KK>, Collection<T>) - Method in interface org.orekit.time.FieldTimeInterpolable

Get an interpolated instance.

interpolate(FieldAbsoluteDate<KK>, Stream<T>) - Method in interface org.orekit.time.FieldTimeInterpolable

Get an interpolated instance.

interpolate(FieldAbsoluteDate<T>, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform

Interpolate a transform from a sample set of existing transforms.

interpolate(FieldAbsoluteDate<T>, Stream<FieldAttitude<T>>) - Method in class org.orekit.attitudes.FieldAttitude

Get an interpolated instance.

interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldCartesianOrbit

Get an interpolated instance.

interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldCircularOrbit

Get an interpolated instance.

interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get an interpolated instance.

interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get an interpolated instance.

interpolate(FieldAbsoluteDate<T>, Stream<FieldSpacecraftState<T>>) - Method in class org.orekit.propagation.FieldSpacecraftState

Get an interpolated instance.

interpolate(FieldAbsoluteDate<T>, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Interpolate angular coordinates.

interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, Collection<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Interpolate position-velocity.

interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, Stream<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Interpolate position-velocity.

interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform

Interpolate a transform from a sample set of existing transforms.

interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Stream<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform

Interpolate a transform from a sample set of existing transforms.

InterpolatingTransformProvider - Class in org.orekit.frames

Transform provider using thread-safe interpolation on transforms sample.

InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider

Simple constructor.

InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider

Deprecated.

as of 9.1, replaced by InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double)

INTERPOLATION - org.orekit.files.ccsds.Keyword

The interpolation method to be used.

INTERPOLATION_DEGREE - org.orekit.files.ccsds.Keyword

The interpolation degree.

InterpolationGrid - Interface in org.orekit.propagation.semianalytical.dsst.utilities

Interface for interpolation grids.

InterpolationTableLoader - Class in org.orekit.utils

Used to read an interpolation table from a data file.

InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader

InterSatDirectViewDetector - Class in org.orekit.propagation.events

Detector for inter-satellites direct view (i.e.

InterSatDirectViewDetector(OneAxisEllipsoid, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.InterSatDirectViewDetector

simple constructor.

InterSatellitesRange - Class in org.orekit.estimation.measurements

One-way or two-way range measurements between two satellites.

InterSatellitesRange(int, int, boolean, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.InterSatellitesRange

Deprecated.

as of 9.3, replaced by InterSatellitesRange(ObservableSatellite, ObservableSatellite, boolean, AbsoluteDate, double, double, double)

InterSatellitesRange(ObservableSatellite, ObservableSatellite, boolean, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.InterSatellitesRange

Simple constructor.

InterSatellitesRangeBuilder - Class in org.orekit.estimation.measurements.generation

Builder for InterSatellitesRange measurements.

InterSatellitesRangeBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, boolean, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder

Simple constructor.

IodGibbs - Class in org.orekit.estimation.iod

Gibbs initial orbit determination.

IodGibbs(double) - Constructor for class org.orekit.estimation.iod.IodGibbs

Creator.

IodGooding - Class in org.orekit.estimation.iod

Gooding angles only initial orbit determination, assuming Keplerian motion.

IodGooding(Frame, double) - Constructor for class org.orekit.estimation.iod.IodGooding

Creator.

IodLambert - Class in org.orekit.estimation.iod

Lambert initial orbit determination, assuming Keplerian motion.

IodLambert(double) - Constructor for class org.orekit.estimation.iod.IodLambert

Creator.

IonosphericModel - Interface in org.orekit.models.earth

Defines a ionospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.

IRNSS - org.orekit.gnss.SatelliteSystem

Indian Regional Navigation Satellite System system.

IRNSS_1GEO - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

IRNSS-1 GEO.

IRNSS_1GEO - org.orekit.gnss.antenna.SatelliteType

IRNSS-1 GEO.

IRNSS_1IGSO - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

IRNSS-1 IGSO.

IRNSS_1IGSO - org.orekit.gnss.antenna.SatelliteType

IRNSS-1 IGSO.

IRNSSScale - Class in org.orekit.time

IRNSS time scale (also called IRNWT for IRNSS NetWork Time).

IRREGULAR_OR_INCOMPLETE_GRID - org.orekit.errors.OrekitMessages

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.FieldAbstractPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.FieldPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator

Check if an additional state is managed.

isChildOf(Frame) - Method in class org.orekit.frames.Frame

Determine if a Frame is a child of another one.

isCurrentStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Determines if the current state is computed directly by the integrator, or if it is calculated using interpolation.

isEnabled() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Check if a measurement is enabled.

isEnabled() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Check if a measurement is enabled.

isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE

Check the lines format validity.

isForward() - Method in class org.orekit.propagation.events.AbstractDetector

Check if the current propagation is forward or backward.

isForward() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Check if the current propagation is forward or backward.

isForward() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Check is integration direction is forward in date.

isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Check is integration direction is forward in date.

isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the Increasing/decreasing status of the event.

isIncreasing() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent

Get the Increasing/decreasing status of the event.

isIncreasing() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event

Is the g() function increasing?

isInertial() - Method in class org.orekit.forces.AbstractParametricAcceleration

Check if direction is inertial.

isInside(Vector3D) - Method in class org.orekit.bodies.Ellipsoid

Check if a point is inside the ellipsoid.

isLof() - Method in enum org.orekit.files.ccsds.CCSDSFrame

Check if the frame is a Local Orbital frame.

isMeanOrbit() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Check if only the mean elements should be used in a semianalitical propagation.

isMeanOrbit() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Check if only the mean elements should be used in a semianalitical propagation.

isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Check if fitting uses only sample positions.

IsotropicDrag - Class in org.orekit.forces.drag

This class models isotropic drag effects.

IsotropicDrag(double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag

Constructor with drag coefficient min/max set to ±∞.

IsotropicDrag(double, double, double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag

Constructor with drag coefficient min/max set by user.

IsotropicRadiationClassicalConvention - Class in org.orekit.forces.radiation

This class represents the features of a simplified spacecraft.

IsotropicRadiationClassicalConvention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Simple constructor.

IsotropicRadiationCNES95Convention - Class in org.orekit.forces.radiation

This class represents the features of a simplified spacecraft.

IsotropicRadiationCNES95Convention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Simple constructor.

IsotropicRadiationSingleCoefficient - Class in org.orekit.forces.radiation

This class represents the features of a simplified spacecraft.

IsotropicRadiationSingleCoefficient(double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Constructor with reflection coefficient min/max set to ±∞.

IsotropicRadiationSingleCoefficient(double, double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Constructor with reflection coefficient min/max set by user.

isPreviousStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Determines if the previous state is computed directly by the integrator, or if it is calculated using interpolation.

isPseudoInertial() - Method in class org.orekit.frames.Frame

Check if the frame is pseudo-inertial.

isSelected() - Method in class org.orekit.utils.ParameterDriver

Check if parameter is selected.

isSimpleEOP() - Method in class org.orekit.files.ccsds.ODMParser

Get EOP interpolation method.

isSimpleEOP() - Method in class org.orekit.files.ccsds.TDMParser

Get EOP interpolation method.

isSupported(String) - Method in class org.orekit.forces.AbstractForceModel

Check if a parameter is supported.

isSupported(String) - Method in interface org.orekit.forces.ForceModel

Check if a parameter is supported.

isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Check if some provider is supported.

isTwoWay() - Method in class org.orekit.estimation.measurements.InterSatellitesRange

Check if the instance represents a two-way measurement.

isTwoWay() - Method in class org.orekit.estimation.measurements.Range

Check if the instance represents a two-way measurement.

isTwoWay() - Method in class org.orekit.estimation.measurements.RangeRate

Check if the instance represents a two-way measurement.

ITRF_2000 - org.orekit.frames.ITRFVersion

Constant for ITRF 2000.

ITRF_2005 - org.orekit.frames.ITRFVersion

Constant for ITRF 2005.

ITRF_2008 - org.orekit.frames.ITRFVersion

Constant for ITRF 2008.

ITRF_2008_TO_ITRF_2000 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 2000.

ITRF_2008_TO_ITRF_2005 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 2005.

ITRF_2008_TO_ITRF_88 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 88.

ITRF_2008_TO_ITRF_89 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 89.

ITRF_2008_TO_ITRF_90 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 90.

ITRF_2008_TO_ITRF_91 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 91.

ITRF_2008_TO_ITRF_92 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 92.

ITRF_2008_TO_ITRF_93 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 93.

ITRF_2008_TO_ITRF_94 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 94.

ITRF_2008_TO_ITRF_96 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 96.

ITRF_2008_TO_ITRF_97 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2008 To ITRF 97.

ITRF_2014 - org.orekit.frames.ITRFVersion

Constant for ITRF 2014.

ITRF_2014_TO_ITRF_2000 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 2000.

ITRF_2014_TO_ITRF_2005 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 2005.

ITRF_2014_TO_ITRF_2008 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 2008.

ITRF_2014_TO_ITRF_88 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 88.

ITRF_2014_TO_ITRF_89 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 89.

ITRF_2014_TO_ITRF_90 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 90.

ITRF_2014_TO_ITRF_91 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 91.

ITRF_2014_TO_ITRF_92 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 92.

ITRF_2014_TO_ITRF_93 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 93.

ITRF_2014_TO_ITRF_94 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 94.

ITRF_2014_TO_ITRF_96 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 96.

ITRF_2014_TO_ITRF_97 - org.orekit.frames.HelmertTransformation.Predefined

Transformation from ITRF 2014 To ITRF 97.

ITRF_88 - org.orekit.frames.ITRFVersion

Constant for ITRF 88.

ITRF_89 - org.orekit.frames.ITRFVersion

Constant for ITRF 89.

ITRF_90 - org.orekit.frames.ITRFVersion

Constant for ITRF 90.

ITRF_91 - org.orekit.frames.ITRFVersion

Constant for ITRF 91.

ITRF_92 - org.orekit.frames.ITRFVersion

Constant for ITRF 92.

ITRF_93 - org.orekit.frames.ITRFVersion

Constant for ITRF 93.

ITRF_94 - org.orekit.frames.ITRFVersion

Constant for ITRF 94.

ITRF_96 - org.orekit.frames.ITRFVersion

Constant for ITRF 96.

ITRF_97 - org.orekit.frames.ITRFVersion

Constant for ITRF 97.

ITRF_CIO_CONV_1996_ACCURATE_EOP - org.orekit.frames.Predefined

CIO-based ITRF, IERS 1996 conventions with accurate EOP interpolation.

ITRF_CIO_CONV_1996_SIMPLE_EOP - org.orekit.frames.Predefined

CIO-based ITRF, IERS 1996 conventions with simple EOP interpolation.

ITRF_CIO_CONV_2003_ACCURATE_EOP - org.orekit.frames.Predefined

CIO-based ITRF, IERS 2003 conventions with accurate EOP interpolation.

ITRF_CIO_CONV_2003_SIMPLE_EOP - org.orekit.frames.Predefined

CIO-based ITRF, IERS 2003 conventions with simple EOP interpolation.

ITRF_CIO_CONV_2010_ACCURATE_EOP - org.orekit.frames.Predefined

CIO-based ITRF, IERS 2010 conventions with accurate EOP interpolation.

ITRF_CIO_CONV_2010_SIMPLE_EOP - org.orekit.frames.Predefined

CIO-based ITRF, IERS 2010 conventions with simple EOP interpolation.

ITRF_EQUINOX_CONV_1996_ACCURATE_EOP - org.orekit.frames.Predefined

Equinox-based ITRF, IERS 1996 conventions with accurate EOP interpolation.

ITRF_EQUINOX_CONV_1996_SIMPLE_EOP - org.orekit.frames.Predefined

Equinox-based ITRF, IERS 1996 conventions with simple EOP interpolation.

ITRF_EQUINOX_CONV_2003_ACCURATE_EOP - org.orekit.frames.Predefined

Equinox-based ITRF, IERS 2003 conventions with accurate EOP interpolation.

ITRF_EQUINOX_CONV_2003_SIMPLE_EOP - org.orekit.frames.Predefined

Equinox-based ITRF, IERS 2003 conventions with simple EOP interpolation.

ITRF_EQUINOX_CONV_2010_ACCURATE_EOP - org.orekit.frames.Predefined

Equinox-based ITRF, IERS 2010 conventions with accurate EOP interpolation.

ITRF_EQUINOX_CONV_2010_SIMPLE_EOP - org.orekit.frames.Predefined

Equinox-based ITRF, IERS 2010 conventions with simple EOP interpolation.

ITRF2000 - org.orekit.files.ccsds.CCSDSFrame

International Terrestrial Reference Frame 2000.

ITRF2005 - org.orekit.files.ccsds.CCSDSFrame

International Terrestrial Reference Frame 2005.

ITRF2008 - org.orekit.files.ccsds.CCSDSFrame

International Terrestrial Reference Frame 2008.

ITRF2014 - org.orekit.files.ccsds.CCSDSFrame

International Terrestrial Reference Frame 2014.

ITRF93 - org.orekit.files.ccsds.CCSDSFrame

International Terrestrial Reference Frame 1993.

ITRF97 - org.orekit.files.ccsds.CCSDSFrame

International Terrestrial Reference Frame 1997.

ITRFVersion - Enum in org.orekit.frames

Enumerate for ITRF versions.

ITRFVersion.Converter - Class in org.orekit.frames

Specialized transform provider between ITRF frames.

J

J01 - org.orekit.gnss.Frequency

QZSS L1 (1575.42 MHz).

J02 - org.orekit.gnss.Frequency

QZSS L2 (1227.6 MHz).

J05 - org.orekit.gnss.Frequency

QZSS L5 (1176.45 MHz).

J06 - org.orekit.gnss.Frequency

QZSS LEX (1278.75 MHz).

J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).

J2000_EPOCH - Static variable in class org.orekit.time.DateComponents

J2000.0 Reference epoch: 2000-01-01.

J2DifferentialEffect - Class in org.orekit.propagation.analytical

Analytical model for J2 effect.

J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

JacobianPropagatorConverter - Class in org.orekit.propagation.conversion

Propagator converter using the real Jacobian.

JacobianPropagatorConverter(NumericalPropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.JacobianPropagatorConverter

Simple constructor.

JacobiansMapper - Class in org.orekit.propagation.numerical

Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.

JacobiPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Provider of the Jacobi polynomials P_l^v,w.

JANUARY - org.orekit.time.Month

January.

JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.

JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents

Java Reference epoch: 1970-01-01.

JB2008 - Class in org.orekit.forces.drag.atmosphere

This is the realization of the Jacchia-Bowman 2008 atmospheric model.

JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.atmosphere.JB2008

Constructor with space environment information for internal computation.

JB2008InputParameters - Interface in org.orekit.forces.drag.atmosphere

Interface for solar activity and magnetic activity data.

JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants

Astronomical Unit: 149597870691 m.

JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants

Earth attraction coefficient (m³/s²).

JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Earth/Moon mass ratio: 81.30059.

JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Earth + Moon) attraction coefficient (m³/s²).

JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants

Gaussian gravitational constant: 0.01720209895 √(AU³/d²).

JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Jupiter system) ttraction coefficient (m³/s²).

JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Mars system) attraction coefficient (m³/s²).

JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants

Sun/Mercury attraction coefficient (m³/s²).

JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants

Moon attraction coefficient (m³/s²).

JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Neptune system) attraction coefficient (m³/s²).

JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Pluto system) ttraction coefficient (m³/s²).

JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Saturn system) attraction coefficient (m³/s²).

JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Earth + Moon) mass ratio: 328900.56.

JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants

Sun attraction coefficient (m³/s²).

JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Jupiter system) mass ratio: 1047.3486.

JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Mars system) mass ratio: 3098708.0.

JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/Mercury mass ratio: 6023600.

JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Neptune system) mass ratio: 19412.24.

JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Pluto system) mass ratio: 1.35e8.

JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Saturn system) mass ratio: 3497.898.

JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Uranus system) mass ratio: 22902.98.

JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/Venus mass ratio: 408523.71.

JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Uranus system) attraction coefficient (m³/s²).

JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants

Sun/Venus attraction coefficient (m³/s²).

JPLEphemeridesLoader - Class in org.orekit.bodies

Loader for JPL ephemerides binary files (DE 4xx) and similar formats (INPOP 06/08/10).

JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader

Create a loader for JPL ephemerides binary files.

JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies

List of supported ephemerides types.

JPLEphemeridesLoader.RawPVProvider - Interface in org.orekit.bodies

Interface for raw position-velocity retrieval.

JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants

Duration of a Julian century: 36525 Constants.JULIAN_DAY.

JULIAN_DAY - Static variable in interface org.orekit.utils.Constants

Duration of a mean solar day: 86400.0 s.

JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.

JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for julian dates: -4712-01-01.

JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants

Duration of a Julian year: 365.25 Constants.JULIAN_DAY.

JULY - org.orekit.time.Month

July.

JUNE - org.orekit.time.Month

June.

JUPITER - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for Jupiter.

JUPITER - org.orekit.files.ccsds.CenterName

Jupiter body.

JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Jupiter.

K

k - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

e_x.

K1 - Static variable in class org.orekit.models.earth.displacement.Tide

K₁ tide.

K2 - Static variable in class org.orekit.models.earth.displacement.Tide

K₂ tide.

KalmanEstimation - Interface in org.orekit.estimation.sequential

Interface for accessing Kalman filter estimations.

KalmanEstimator - Class in org.orekit.estimation.sequential

Implementation of a Kalman filter to perform orbit determination.

KalmanEstimatorBuilder - Class in org.orekit.estimation.sequential

Builder for a Kalman filter estimator.

KalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Default constructor.

KalmanObserver - Interface in org.orekit.estimation.sequential

Observer for Kalman filter estimations.

KEPLERIAN - org.orekit.orbits.OrbitType

Type for propagation in Keplerian parameters.

KeplerianOrbit - Class in org.orekit.orbits

This class handles traditional Keplerian orbital parameters.

KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Creates a new instance.

KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Creates a new instance.

KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from any kind of orbital parameters.

KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from Cartesian parameters.

KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from Cartesian parameters.

KeplerianPropagator - Class in org.orekit.propagation.analytical

Simple Keplerian orbit propagator.

KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit only.

KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit and central attraction coefficient μ.

KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit and attitude provider.

KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit, attitude provider and central attraction coefficient μ.

KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for Keplerian propagator.

KeplerianPropagatorBuilder(Orbit, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Build a new instance.

KEYVALUE - org.orekit.files.ccsds.TDMParser.TDMFileFormat

Keyvalue (text file with Key = Value lines).

Keyword - Enum in org.orekit.files.ccsds

Keywords for CCSDS Navigation Data Messages.

KLOBUCHAR_ALPHA_BETA_NOT_AVAILABLE_FOR_DATE - org.orekit.errors.OrekitMessages

KLOBUCHAR_ALPHA_BETA_NOT_LOADED - org.orekit.errors.OrekitMessages

KlobucharIonoCoefficientsLoader - Class in org.orekit.models.earth

Loads Klobuchar-Style ionospheric coefficients a given input stream.

KlobucharIonoCoefficientsLoader() - Constructor for class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Constructor with default supported names.

KlobucharIonoCoefficientsLoader(String) - Constructor for class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Constructor with supported names given by user.

KlobucharIonoModel - Class in org.orekit.models.earth

Klobuchar ionospheric delay model.

KlobucharIonoModel(double[], double[]) - Constructor for class org.orekit.models.earth.KlobucharIonoModel

Create a new Klobuchar ionospheric delay model, when single L1 frequency system is used.

KlobucharIonoModel(double[], double[], double) - Constructor for class org.orekit.models.earth.KlobucharIonoModel

Create a new Klobuchar ionospheric delay model, when a single frequency system is used.

L

L1 - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.

L1A - org.orekit.gnss.ObservationType

Carrier-phase Galileo E1 A for Rinex3.

L1B - org.orekit.gnss.ObservationType

Carrier-phase Galileo E1 I/NAV OS/CS/SoL for Rinex3.

L1C - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.

L1Frame - Class in org.orekit.frames

Class to create a L1 centered frame with L1TransformProvider.

L1Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1Frame

Simple constructor.

L1I - org.orekit.gnss.ObservationType

Carrier-phase Beidou B1 I for Rinex3.

L1L - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3.

L1M - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 M for Rinex3.

L1N - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 codeless for Rinex3.

L1P - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 P(AS off) / GLONASS G2 P for Rinex3.

L1S - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3.

L1TransformProvider - Class in org.orekit.frames

L1 Transform provider for a frame on the L1 Lagrange point of two celestial bodies.

L1TransformProvider(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1TransformProvider

Simple constructor.

L1W - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 Z-tracking and similar (AS on) for Rinex3.

L1X - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) for Rinex3.

L1Y - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 Y for Rinex3.

L1Z - org.orekit.gnss.ObservationType

Carrier-phase Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3.

L2 - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.

L2C - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 C/A / GLONASS G2 C/A for Rinex3.

L2D - org.orekit.gnss.ObservationType

Carrier-phase GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.

L2Frame - Class in org.orekit.frames

Class to create a L2 centered frame with L2TransformProvider.

L2Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L2Frame

Simple constructor.

L2I - org.orekit.gnss.ObservationType

Carrier-phase Beidou B1 I for Rinex3.03.

L2L - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.

L2M - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 M for Rinex3.

L2N - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 codeless for Rinex3.

L2P - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 P(AS off) / GLONASS G2 P for Rinex3.

L2Q - org.orekit.gnss.ObservationType

Carrier-phase Beidou B1 Q for Rinex3.03.

L2S - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.

L2W - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 Z-tracking and similar (AS on) for Rinex3.

L2X - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3.

L2Y - org.orekit.gnss.ObservationType

Carrier-phase GPS L2 Y for Rinex3.

L3I - org.orekit.gnss.ObservationType

Carrier-phase GLONASS G3 I for Rinex3.

L3Q - org.orekit.gnss.ObservationType

Carrier-phase GLONASS G3 Q for Rinex3.

L3X - org.orekit.gnss.ObservationType

Carrier-phase GLONASS G3 I+Q for Rinex3.

L5 - org.orekit.gnss.ObservationType

Carrier-phase GPS L5 / Galileo E5a / SBAS L5 for Rinex2.

L5A - org.orekit.gnss.ObservationType

Carrier-phase IRNSS L5 A for Rinex3.

L5B - org.orekit.gnss.ObservationType

Carrier-phase IRNSS L5 B for Rinex3.

L5C - org.orekit.gnss.ObservationType

Carrier-phase IRNSS L5 C for Rinex3.

L5I - org.orekit.gnss.ObservationType

Carrier-phase GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.

L5Q - org.orekit.gnss.ObservationType

Carrier-phase GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.

L5X - org.orekit.gnss.ObservationType

Carrier-phase GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C for Rinex3.

L6 - org.orekit.gnss.ObservationType

Carrier-phase Galileo E6 / Beidou B03 for Rinex2.

L6A - org.orekit.gnss.ObservationType

Carrier-phase Galileo E6 A PRS for Rinex3.

L6B - org.orekit.gnss.ObservationType

Carrier-phase Galileo E6 B C/NAV CS for Rinex3.

L6C - org.orekit.gnss.ObservationType

Carrier-phase Galileo E6 C no data for Rinex3.

L6I - org.orekit.gnss.ObservationType

Carrier-phase Beidou B3 I for Rinex3.

L6L - org.orekit.gnss.ObservationType

Carrier-phase QZSS LEX(6) L for Rinex3.

L6Q - org.orekit.gnss.ObservationType

Carrier-phase Beidou B3 Q for Rinex3.

L6S - org.orekit.gnss.ObservationType

Carrier-phase QZSS LEX(6) S for Rinex3.

L6X - org.orekit.gnss.ObservationType

Carrier-phase Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q for Rinex3.

L6Z - org.orekit.gnss.ObservationType

Carrier-phase Galileo E6 A+B+C for Rinex3.

L7 - org.orekit.gnss.ObservationType

Carrier-phase Galileo E5b / Beidou B02 for Rinex2.

L7I - org.orekit.gnss.ObservationType

Carrier-phase Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.

L7Q - org.orekit.gnss.ObservationType

Carrier-phase Galileo Q no data / Beidou B2 Q for Rinex3.

L7X - org.orekit.gnss.ObservationType

Carrier-phase Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.

L8 - org.orekit.gnss.ObservationType

Carrier-phase Galileo E5a+b for Rinex2.

L8I - org.orekit.gnss.ObservationType

Carrier-phase Galileo E5(E5a+E5b) I for Rinex3.

L8Q - org.orekit.gnss.ObservationType

Carrier-phase Galileo E5(E5a+E5b) Q for Rinex3.

L8X - org.orekit.gnss.ObservationType

Carrier-phase Galileo E5(E5a+E5b) I+Q for Rinex3.

L9A - org.orekit.gnss.ObservationType

Carrier-phase IRNSS S A for Rinex3.

L9B - org.orekit.gnss.ObservationType

Carrier-phase IRNSS S B for Rinex3.

L9C - org.orekit.gnss.ObservationType

Carrier-phase IRNSS S C for Rinex3.

L9X - org.orekit.gnss.ObservationType

Carrier-phase IRNSS S B+C for Rinex3.

LA - org.orekit.gnss.ObservationType

Carrier-phase GPS L1 C/A / GLONASS G1 C/A for Rinex2.

LAGRANGE - org.orekit.files.ccsds.OEMWriter.InterpolationMethod

Lagrange interpolation.

LatitudeCrossingDetector - Class in org.orekit.propagation.events

Detector for geographic latitude crossing.

LatitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector

Build a detector.

LatitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector

Build a new detector.

LatitudeExtremumDetector - Class in org.orekit.propagation.events

Detector for geographic latitude extremum.

LatitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector

Build a detector.

LatitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector

Build a new detector.

LB - org.orekit.gnss.ObservationType

Carrier-phase GPS L1C for Rinex2.

LC - org.orekit.gnss.ObservationType

Carrier-phase GPS L2C for Rinex2.

LD - org.orekit.gnss.ObservationType

Carrier-phase GLONASS G2 for Rinex2.

LEO - org.orekit.files.sp3.SP3File.SP3FileType

LEO only file.

LIFT_RATIO - Static variable in interface org.orekit.forces.drag.DragSensitive

Parameter name for lift ration enabling Jacobian processing.

LINEAR - org.orekit.files.ccsds.OEMWriter.InterpolationMethod

Linear interpolation.

lm - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Mean longitude.

LnsCoefficients - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the L_n^s(γ).

LnsCoefficients(int, int, double[][], TreeMap<CoefficientsFactory.NSKey, Double>, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Create a set of L_n^s(γ) coefficients.

loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader

Load celestial body.

loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader

Load celestial body.

loadData() - Method in class org.orekit.gnss.SEMParser

Loads almanacs.

loadData() - Method in class org.orekit.gnss.YUMAParser

Loads almanacs.

loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCHatEpsilonReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCnmSnmReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.gnss.RinexLoader.Parser

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.gnss.SEMParser

loadData(InputStream, String) - Method in class org.orekit.gnss.YUMAParser

loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Load Klobuchar-Style ionospheric coefficients read from some file.

loadData(InputStream, String) - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader

loadData(InputStream, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.utils.InterpolationTableLoader

Loads an bi-variate interpolation table from the given InputStream.

loadKlobucharIonosphericCoefficients() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Load the data using supported names .

loadKlobucharIonosphericCoefficients(DateComponents) - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Load the data for a given day.

loadLoveNumbers(String) - Method in enum org.orekit.utils.IERSConventions

Load the Love numbers.

loadOffsets() - Method in class org.orekit.time.TAIUTCDatFilesLoader

Load UTC-TAI offsets entries.

loadOffsets() - Method in class org.orekit.time.UTCTAIBulletinAFilesLoader

Load UTC-TAI offsets entries.

loadOffsets() - Method in class org.orekit.time.UTCTAIHistoryFilesLoader

Load UTC-TAI offsets entries.

loadOffsets() - Method in interface org.orekit.time.UTCTAIOffsetsLoader

Load UTC-TAI offsets entries.

loadTLEData() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Load TLE data for a specified object.

loadTLEData(int) - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Load TLE data for a specified object.

loadTLEData(int, int, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Load TLE data for a specified object.

loadViennaCoefficients() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader

Load the data using supported names .

loadViennaCoefficients(DateTimeComponents) - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader

Load the data for a given day.

LocalizedException - Interface in org.orekit.errors

This interface specified methods implemented by localized exception classes.

LocalOrbitalFrame - Class in org.orekit.frames

Class for frames moving with an orbiting satellite.

LocalOrbitalFrame(Frame, LOFType, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame

Build a new instance.

LofOffset - Class in org.orekit.attitudes

Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.

LofOffset(Frame, LOFType) - Constructor for class org.orekit.attitudes.LofOffset

Create a LOF-aligned attitude.

LofOffset(Frame, LOFType, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset

Creates new instance.

LofOffsetPointing - Class in org.orekit.attitudes

This class provides a default attitude provider.

LofOffsetPointing(Frame, BodyShape, AttitudeProvider, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing

Creates new instance.

LOFType - Enum in org.orekit.frames

Enumerate for different types of Local Orbital Frames.

LongitudeCrossingDetector - Class in org.orekit.propagation.events

Detector for geographic longitude crossing.

LongitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector

Build a detector.

LongitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector

Build a new detector.

LongitudeExtremumDetector - Class in org.orekit.propagation.events

Detector for geographic longitude extremum.

LongitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector

Build a detector.

LongitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector

Build a new detector.

LoveNumbers - Class in org.orekit.utils

Container for Love numbers.

LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers

Simple constructor.

luniSolarTermsComputation() - Method in class org.orekit.propagation.analytical.tle.DeepSDP4

Computes luni - solar terms from initial coordinates and epoch.

LutherIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for LutherIntegrator.

LutherIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.LutherIntegratorBuilder

Build a new instance.

LVLH - org.orekit.frames.LOFType

Constant for Local Vertical, Local Horizontal frame (X axis aligned with position, Z axis aligned with orbital momentum).

M

M2 - Static variable in class org.orekit.models.earth.displacement.Tide

M₂ tide.

MAN_DELTA_MASS - org.orekit.files.ccsds.Keyword

Mass change during maneuver (value is < 0).

MAN_DURATION - org.orekit.files.ccsds.Keyword

Maneuver duration (If = 0, impulsive maneuver).

MAN_DV_1 - org.orekit.files.ccsds.Keyword

First component of the velocity increment.

MAN_DV_2 - org.orekit.files.ccsds.Keyword

Second component of the velocity increment.

MAN_DV_3 - org.orekit.files.ccsds.Keyword

Third component of the velocity increment.

MAN_EPOCH_IGNITION - org.orekit.files.ccsds.Keyword

Epoch of ignition.

MAN_REF_FRAME - org.orekit.files.ccsds.Keyword

Coordinate system for velocity increment vector.

Maneuver() - Constructor for class org.orekit.files.ccsds.OPMFile.Maneuver

Simple constructor.

mapArrayToOrbit(double[], double[], PositionAngle, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType

Convert state array to orbital parameters.

mapArrayToOrbit(T[], T[], PositionAngle, FieldAbsoluteDate<T>, double, Frame) - Method in enum org.orekit.orbits.OrbitType

Convert state array to orbital parameters.

mapArrayToState(double, double[], double[], boolean) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double components to a spacecraft state.

mapArrayToState(AbsoluteDate, double[], double[], boolean) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double components to a spacecraft state.

mapArrayToState(FieldAbsoluteDate<T>, T[], T[], boolean) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map the raw double components to a spacecraft state.

mapArrayToState(T, T[], T[], boolean) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map the raw double components to a spacecraft state.

mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper

Map a date to a raw double time offset.

mapDateToDouble(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map a date to a raw double time offset.

mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double time offset to a date.

mapDoubleToDate(double, AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double time offset to a date.

mapDoubleToDate(T) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map the raw double time offset to a date.

mapDoubleToDate(T, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map the raw double time offset to a date.

mapOrbitToArray(FieldOrbit<T>, PositionAngle, T[], T[]) - Method in enum org.orekit.orbits.OrbitType

Convert orbit to state array.

mapOrbitToArray(Orbit, PositionAngle, double[], double[]) - Method in enum org.orekit.orbits.OrbitType

Convert orbit to state array.

mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.EstimatedTroposphericModel

mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.GlobalMappingFunctionModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.MappingFunction

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.MendesPavlisModel

With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.

mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.NiellMappingFunctionModel

mappingFactors(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.TroposphericModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaOneModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaThreeModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.EstimatedTroposphericModel

mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.GlobalMappingFunctionModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.MappingFunction

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.MendesPavlisModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.NiellMappingFunctionModel

mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.TroposphericModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaOneModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaThreeModel

This method allows the computation of the hydrostatic and wet mapping functions.

MappingFunction - Interface in org.orekit.models.earth

Interface for mapping functions used in the tropospheric delay computation.

mapStateToArray(FieldSpacecraftState<T>, T[], T[]) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map a spacecraft state to raw double components.

mapStateToArray(SpacecraftState, double[], double[]) - Method in class org.orekit.propagation.integration.StateMapper

Map a spacecraft state to raw double components.

MARCH - org.orekit.time.Month

March.

MariniMurrayModel - Class in org.orekit.models.earth

The Marini-Murray tropospheric delay model for laser ranging.

MariniMurrayModel(double, double, double, double, double) - Constructor for class org.orekit.models.earth.MariniMurrayModel

Create a new Marini-Murray model for the troposphere using the given environmental conditions.

MARS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for Mars.

MARS - org.orekit.files.ccsds.CenterName

Mars body.

MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Mars.

MarshallSolarActivityFutureEstimation - Class in org.orekit.forces.drag.atmosphere.data

This class reads and provides solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.

MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Simple constructor.

MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.forces.drag.atmosphere.data

Strength level of activity.

mass(double) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder

Sets the mass.

MASS - org.orekit.files.ccsds.Keyword

Spacecraft mass.

MASTER_MODE - Static variable in interface org.orekit.propagation.FieldPropagator

Indicator for master mode.

MASTER_MODE - Static variable in interface org.orekit.propagation.Propagator

Indicator for master mode.

MAX_EPOCH - Static variable in class org.orekit.time.DateComponents

Maximum supported date.

MaxGapInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolation grid where points obey a maximum time gap.

MaxGapInterpolationGrid(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid

Constructor.

maxValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter maximum value has been changed.

MAY - org.orekit.time.Month

May.

MCI - org.orekit.files.ccsds.CCSDSFrame

Mars Centered Inertial.

MEAN - org.orekit.orbits.PositionAngle

Mean angle.

MEAN_ANOMALY - org.orekit.files.ccsds.Keyword

Orbit mean anomaly.

MEAN_ELEMENT_THEORY - org.orekit.files.ccsds.Keyword

Mean element theory.

MEAN_MOTION - org.orekit.files.ccsds.Keyword

Mean Motion.

MEAN_MOTION_DDOT - org.orekit.files.ccsds.Keyword

Second Time Derivative of the Mean Motion.

MEAN_MOTION_DOT - org.orekit.files.ccsds.Keyword

First Time Derivative of the Mean Motion.

meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean derivative, truncated to first components.

meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean second derivative, truncated to first components.

meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit

Computes the eccentric latitude argument from the mean latitude argument.

meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit

Computes the eccentric longitude argument from the mean longitude argument.

meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Computes the eccentric latitude argument from the mean latitude argument.

meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Computes the eccentric longitude argument from the mean longitude argument.

meanToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit

Computes the elliptic eccentric anomaly from the mean anomaly.

meanToEllipticEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Computes the elliptic eccentric anomaly from the mean anomaly.

meanToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit

Computes the hyperbolic eccentric anomaly from the mean anomaly.

meanToHyperbolicEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Computes the hyperbolic eccentric anomaly from the mean anomaly.

meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean value, truncated to first components.

MeasurementBuilder<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation

Interface for generating individual measurements.

MeasurementDecorator - Class in org.orekit.estimation.sequential

Decorator adding Measurement API to an ObservedMeasurement.

MeasurementDecorator(ObservedMeasurement<?>, RealMatrix, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.MeasurementDecorator

Simple constructor.

measurementIsFeasible(double) - Method in enum org.orekit.estimation.measurements.generation.SignSemantic

Check if measurement is feasible.

MeasurementType - Enum in org.orekit.gnss

Enumerate for measurement type.

MendesPavlisModel - Class in org.orekit.models.earth

The Mendes - Pavlis tropospheric delay model for optical techniques.

MendesPavlisModel(double, double, double, double, double) - Constructor for class org.orekit.models.earth.MendesPavlisModel

Create a new Mendes-Pavlis model for the troposphere.

MERCURY - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for Mercury.

MERCURY - org.orekit.files.ccsds.CenterName

Mercury body.

MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Mercury.

MET - org.orekit.files.ccsds.CcsdsTimeScale

Mission Elapsed Time.

META_START - org.orekit.files.ccsds.Keyword

Keyword used to delineate the start of a Meta-data block.

META_STOP - org.orekit.files.ccsds.Keyword

Keyword used to delineate the end of a Meta-data block.

metadata - org.orekit.files.ccsds.Keyword

Meta-data keyword.

MF - Static variable in class org.orekit.models.earth.displacement.Tide

Mf tide.

MICRO_ARC_SECONDS - org.orekit.data.PolynomialParser.Unit

Micro arc-seconds angles.

MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for MidpointIntegrator.

MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder

Build a new instance.

MILLI_ARC_SECONDS - org.orekit.data.PolynomialParser.Unit

Milli arc-seconds angles.

MIN_EPOCH - Static variable in class org.orekit.time.DateComponents

Maximum supported date.

minuteDuration(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale

Check length of the current minute in this time scale.

minuteDuration(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Check length of the current minute in this time scale.

minuteDuration(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Check length of the current minute in this time scale.

minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale

Check length of the current minute in this time scale.

minuteDuration(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale

Check length of the current minute in this time scale.

minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale

Check length of the current minute in this time scale.

minValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter minimum value has been changed.

MISMATCHED_FREQUENCIES - org.orekit.errors.OrekitMessages

MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES - org.orekit.errors.OrekitMessages

MISSING_GRAVITY_FIELD_COEFFICIENT_IN_FILE - org.orekit.errors.OrekitMessages

MISSING_SECOND_TLE_LINE - org.orekit.errors.OrekitMessages

MISSING_SERIE_J_IN_FILE - org.orekit.errors.OrekitMessages

missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Check if missing coefficients are allowed in the input data.

MIXED - org.orekit.files.sp3.SP3File.SP3FileType

Mixed file.

MIXED - org.orekit.gnss.SatelliteSystem

Mixed system.

MM - Static variable in class org.orekit.models.earth.displacement.Tide

Mm tide.

MOD_CONVENTIONS_1996 - org.orekit.frames.Predefined

MOD, IERS 1996 conventions.

MOD_CONVENTIONS_2003 - org.orekit.frames.Predefined

MOD, IERS 2003 conventions.

MOD_CONVENTIONS_2010 - org.orekit.frames.Predefined

MOD, IERS 2010 conventions.

MOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined

MOD, IERS 1996 conventions without EOP corrections.

MODE - org.orekit.files.ccsds.Keyword

Meta-data: Tracking mode associated with data section of the segment.

ModeHandler - Interface in org.orekit.propagation.integration

Common interface for all propagator mode handlers initialization.

Model - Class in org.orekit.estimation.sequential

Class defining the process model dynamics to use with a KalmanEstimator.

MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.

MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for modified julian dates: 1858-11-17.

modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier

modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier

modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier

modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier

modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier

modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier

modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.Bias

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter

Apply a modifier to an estimated measurement.

MOLECULAR_NITROGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000

Identifier for molecular nitrogen.

MOLECULAR_OXYGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000

Identifier for molecular oxygen.

monitorDetector(D) - Method in class org.orekit.propagation.events.FieldEventsLogger

Monitor an event detector.

monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger

Monitor an event detector.

Month - Enum in org.orekit.time

Enumerate representing a calendar month.

MOON - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for the Moon.

MOON - org.orekit.files.ccsds.CenterName

Moon body.

MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Moon.

MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Moon equatorial radius: 1737400 m.

MRT - org.orekit.files.ccsds.CcsdsTimeScale

Mission Relative Time.

mu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

μ .

multiply(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Multiply the argument matrix with the current matrix.

MultiSatStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step handler for multi-sat propagation.

N

n - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Kepler mean motion: n = sqrt(μ / a³).

N2 - Static variable in class org.orekit.models.earth.displacement.Tide

N₂ tide.

NadirPointing - Class in org.orekit.attitudes

This class handles nadir pointing attitude provider.

NadirPointing(Frame, BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing

Creates new instance.

nameChanged(String, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter name has been changed.

NamedData - Class in org.orekit.data

Container for holding named data that can be filtered.

NamedData(String, NamedData.StreamOpener) - Constructor for class org.orekit.data.NamedData

Simple constructor.

NamedData.StreamOpener - Interface in org.orekit.data

Interface for lazy-opening a stream.

NAUTICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector

Sun elevation at nautical dawn/dusk (12° below horizon).

negate() - Method in class org.orekit.utils.FieldPVCoordinates

Get the opposite of the instance.

negate() - Method in class org.orekit.utils.PVCoordinates

Get the opposite of the instance.

NegateDetector - Class in org.orekit.propagation.events

An event detector that negates the sign on another event detector's g function.

NegateDetector(EventDetector) - Constructor for class org.orekit.propagation.events.NegateDetector

Create a new event detector that negates an existing event detector.

NEITHER_DIRECTORY_NOR_ZIP_OR_JAR - org.orekit.errors.OrekitMessages

NEPTUNE - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for Neptune.

NEPTUNE - org.orekit.files.ccsds.CenterName

Neptune body.

NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Neptune.

NetworkCrawler - Class in org.orekit.data

Provider for data files directly fetched from network.

NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler

Build a data classpath crawler.

newBundle(String, Locale, String, ClassLoader, boolean) - Method in class org.orekit.errors.OrekitMessages.UTF8Control

NewcombOperators - Class in org.orekit.propagation.semianalytical.dsst.utilities

Implementation of the Modified Newcomb Operators.

newSegment(Frame, Map<Keyword, String>) - Method in class org.orekit.files.ccsds.StreamingOemWriter

Create a writer for a new OEM ephemeris segment.

NewtonianAttraction - Class in org.orekit.forces.gravity

Force model for Newtonian central body attraction.

NewtonianAttraction(double) - Constructor for class org.orekit.forces.gravity.NewtonianAttraction

Simple constructor.

NiellMappingFunctionModel - Class in org.orekit.models.earth

The Niell Mapping Function model for radio wavelengths.

NiellMappingFunctionModel(double) - Constructor for class org.orekit.models.earth.NiellMappingFunctionModel

Buils a new instance.

NO_CACHED_ENTRIES - org.orekit.errors.OrekitMessages

NO_DATA_GENERATED - org.orekit.errors.OrekitMessages

NO_DATA_LOADED_FOR_CELESTIAL_BODY - org.orekit.errors.OrekitMessages

NO_EARTH_ORIENTATION_PARAMETERS - org.orekit.errors.OrekitMessages

NO_EARTH_ORIENTATION_PARAMETERS_LOADED - org.orekit.errors.OrekitMessages

NO_ENTRIES_IN_IERS_UTC_TAI_HISTORY_FILE - org.orekit.errors.OrekitMessages

NO_GRAVITY_FIELD_DATA_LOADED - org.orekit.errors.OrekitMessages

NO_IERS_UTC_TAI_HISTORY_DATA_LOADED - org.orekit.errors.OrekitMessages

NO_JPL_EPHEMERIDES_BINARY_FILES_FOUND - org.orekit.errors.OrekitMessages

NO_KLOBUCHAR_ALPHA_BETA_IN_FILE - org.orekit.errors.OrekitMessages

NO_OCEAN_TIDE_DATA_LOADED - org.orekit.errors.OrekitMessages

NO_PROPAGATOR_CONFIGURED - org.orekit.errors.OrekitMessages

NO_REFERENCE_DATE_FOR_PARAMETER - org.orekit.errors.OrekitMessages

NO_SEM_ALMANAC_AVAILABLE - org.orekit.errors.OrekitMessages

NO_SOLAR_ACTIVITY_AT_DATE - org.orekit.errors.OrekitMessages

NO_SUCH_ITRF_FRAME - org.orekit.errors.OrekitMessages

NO_TLE_DATA_AVAILABLE - org.orekit.errors.OrekitMessages

NO_TLE_FOR_LAUNCH_YEAR_NUMBER_PIECE - org.orekit.errors.OrekitMessages

NO_TLE_FOR_OBJECT - org.orekit.errors.OrekitMessages

NO_UNITS - org.orekit.data.PolynomialParser.Unit

No units.

NO_VIENNA_ACOEF_OR_ZENITH_DELAY_IN_FILE - org.orekit.errors.OrekitMessages

NO_YUMA_ALMANAC_AVAILABLE - org.orekit.errors.OrekitMessages

NodeDetector - Class in org.orekit.propagation.events

Finder for node crossing events.

NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector

Build a new instance.

NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector

Build a new instance.

NON_CHRONOLOGICAL_DATES_IN_FILE - org.orekit.errors.OrekitMessages

NON_CHRONOLOGICALLY_SORTED_ENTRIES - org.orekit.errors.OrekitMessages

NON_EXISTENT_DATE - org.orekit.errors.OrekitMessages

NON_EXISTENT_DAY_NUMBER_IN_YEAR - org.orekit.errors.OrekitMessages

NON_EXISTENT_GEOMAGNETIC_MODEL - org.orekit.errors.OrekitMessages

NON_EXISTENT_HMS_TIME - org.orekit.errors.OrekitMessages

NON_EXISTENT_MONTH - org.orekit.errors.OrekitMessages

NON_EXISTENT_TIME - org.orekit.errors.OrekitMessages

NON_EXISTENT_WEEK_DATE - org.orekit.errors.OrekitMessages

NON_EXISTENT_YEAR_MONTH_DAY - org.orekit.errors.OrekitMessages

NON_PSEUDO_INERTIAL_FRAME - org.orekit.errors.OrekitMessages

NON_RESETABLE_STATE - org.orekit.errors.OrekitMessages

nonCentralPart(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the non-central part of the gravity field.

NORAD_CAT_ID - org.orekit.files.ccsds.Keyword

NORAD catalogue number.

normalize() - Method in class org.orekit.utils.FieldPVCoordinates

Normalize the position part of the instance.

normalize() - Method in class org.orekit.utils.PVCoordinates

Normalize the position part of the instance.

normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Normalize an angle in a 2π wide interval around a center value.

normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Normalize an angle in a 2π wide interval around a center value.

normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Normalize an angle in a 2π wide interval around a center value.

normalizeAngle(T, T) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Normalize an angle in a 2π wide interval around a center value.

NormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide normalized spherical harmonics coefficients.

NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

The normalized geopotential coefficients at a specific instance in time.

NOT_A_DIRECTORY - org.orekit.errors.OrekitMessages

NOT_A_JPL_EPHEMERIDES_BINARY_FILE - org.orekit.errors.OrekitMessages

NOT_A_MARSHALL_SOLAR_ACTIVITY_FUTURE_ESTIMATION_FILE - org.orekit.errors.OrekitMessages

NOT_A_SUPPORTED_IERS_DATA_FILE - org.orekit.errors.OrekitMessages

NOT_A_SUPPORTED_SEM_ALMANAC_FILE - org.orekit.errors.OrekitMessages

NOT_A_SUPPORTED_UNIX_COMPRESSED_FILE - org.orekit.errors.OrekitMessages

NOT_A_SUPPORTED_YUMA_ALMANAC_FILE - org.orekit.errors.OrekitMessages

NOT_ENOUGH_CACHED_NEIGHBORS - org.orekit.errors.OrekitMessages

NOT_ENOUGH_DATA_FOR_INTERPOLATION - org.orekit.errors.OrekitMessages

NOT_ENOUGH_GNSS_FOR_DOP - org.orekit.errors.OrekitMessages

NOT_ENOUGH_PROPAGATORS - org.orekit.errors.OrekitMessages

NOT_POSITIVE_SPACECRAFT_MASS - org.orekit.errors.OrekitMessages

NOT_TLE_LINES - org.orekit.errors.OrekitMessages

notCombine(EventDetector) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that negates the g function of another detector.

NOVEMBER - org.orekit.time.Month

November.

NRLMSISE00 - Class in org.orekit.forces.drag.atmosphere

This class implements the mathematical representation of the 2001 Naval Research Laboratory Mass Spectrometer and Incoherent Scatter Radar Exosphere (NRLMSISE-00) of the MSIS® class model.

NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.atmosphere.NRLMSISE00

Constructor.

NRLMSISE00.FieldOutput<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.forces.drag.atmosphere

This class is a placeholder for the computed densities and temperatures.

NRLMSISE00InputParameters - Interface in org.orekit.forces.drag.atmosphere

Container for solar activity data, compatible with NRLMSISE-00 atmosphere model.

NSKey(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

Simple constructor.

NULL_ARGUMENT - org.orekit.errors.OrekitMessages

NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection

Null correction (xp = 0, yp = 0).

NULL_PARENT_FOR_FRAME - org.orekit.errors.OrekitMessages

NumericalPropagator - Class in org.orekit.propagation.numerical

This class propagates orbits using numerical integration.

NumericalPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator

Create a new instance of NumericalPropagator, based on orbit definition mu.

NumericalPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for numerical propagator.

NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Build a new instance.

O

O1 - Static variable in class org.orekit.models.earth.displacement.Tide

O₁ tide.

OBJECT_ID - org.orekit.files.ccsds.Keyword

Object identifier of the object for which the orbit state is provided.

OBJECT_NAME - org.orekit.files.ccsds.Keyword

Spacecraft name for which the orbit state is provided.

ObservableSatellite - Class in org.orekit.estimation.measurements

Class modeling a satellite that can be observed.

ObservableSatellite(int) - Constructor for class org.orekit.estimation.measurements.ObservableSatellite

Simple constructor.

observation - org.orekit.files.ccsds.Keyword

Observation keyword.

ObservationData - Class in org.orekit.gnss

Observation Data.

ObservationData(ObservationType, double, int, int) - Constructor for class org.orekit.gnss.ObservationData

Simple constructor.

ObservationDataSet - Class in org.orekit.gnss

Observation Data set.

ObservationDataSet(RinexHeader, SatelliteSystem, int, AbsoluteDate, double, List<ObservationData>) - Constructor for class org.orekit.gnss.ObservationDataSet

Simple constructor.

ObservationsBlock() - Constructor for class org.orekit.files.ccsds.TDMFile.ObservationsBlock

ObservationsBlock constructor.

ObservationType - Enum in org.orekit.gnss

Enumerate for all the Observation Types for Rinex 2 and 3.

ObservedMeasurement<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements

Interface for measurements used for orbit determination.

OCEAN_TIDE_DATA_DEGREE_ORDER_LIMITS - org.orekit.errors.OrekitMessages

OCEAN_TIDE_LOAD_DEFORMATION_LIMITS - org.orekit.errors.OrekitMessages

OceanLoadDeformationCoefficients - Enum in org.orekit.forces.gravity.potential

Supported Ocean load Deformation coefficients (Love numbers k'_i).

OceanLoading - Class in org.orekit.models.earth.displacement

Modeling of displacement of reference points due to ocean loading.

OceanLoading(OneAxisEllipsoid, OceanLoadingCoefficients) - Constructor for class org.orekit.models.earth.displacement.OceanLoading

Simple constructor.

OceanLoadingCoefficients - Class in org.orekit.models.earth.displacement

Site specific coefficients for ocean loading.

OceanLoadingCoefficients(String, GeodeticPoint, Tide[][], double[][], double[][], double[][], double[][], double[][], double[][]) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Simple constructor.

OceanLoadingCoefficientsBLQFactory - Class in org.orekit.models.earth.displacement

Factory for ocean loading coefficients, using Onsala Space Observatory files in BLQ format.

OceanLoadingCoefficientsBLQFactory(String) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

Simple constructor.

OceanTides - Class in org.orekit.forces.gravity

Ocean tides force model.

OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides

Simple constructor.

OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides

Simple constructor.

OceanTidesReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides coefficients.

OceanTidesReader(String) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesReader

Simple constructor.

OceanTidesWave - Class in org.orekit.forces.gravity.potential

Container for ocen tides coefficients for one tide wave.

OceanTidesWave(int, int, int, double[][][]) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesWave

Simple constructor.

OCTOBER - org.orekit.time.Month

October.

ODEIntegratorBuilder - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction to build first order integrators for propagators conversion.

ODMFile - Class in org.orekit.files.ccsds

The ODMFile (Orbit Data Message) class represents any of the three orbit messages used by the CCSDS, i.e.

ODMFile() - Constructor for class org.orekit.files.ccsds.ODMFile

ODMFile constructor.

ODMMetaData - Class in org.orekit.files.ccsds

This class gathers the meta-data present in the Orbital Data Message (ODM).

ODMParser - Class in org.orekit.files.ccsds

Base class for all CCSDS Orbit Data Message parsers.

ODMParser(AbsoluteDate, double, IERSConventions, boolean, int, int, String) - Constructor for class org.orekit.files.ccsds.ODMParser

Complete constructor.

OEMFile - Class in org.orekit.files.ccsds

This class stocks all the information of the OEM File parsed by OEMParser.

OEMFile() - Constructor for class org.orekit.files.ccsds.OEMFile

OEMFile constructor.

OEMFile.CovarianceMatrix - Class in org.orekit.files.ccsds

The CovarianceMatrix class represents a covariance matrix and its metadata: epoch and frame.

OEMFile.EphemeridesBlock - Class in org.orekit.files.ccsds

The Ephemerides Blocks class contain metadata, the list of ephemerides data lines and optional covariance matrices (and their metadata).

OEMFile.OemSatelliteEphemeris - Class in org.orekit.files.ccsds

OEM ephemeris blocks for a single satellite.

OEMParser - Class in org.orekit.files.ccsds

A parser for the CCSDS OEM (Orbit Ephemeris Message).

OEMParser() - Constructor for class org.orekit.files.ccsds.OEMParser

Simple constructor.

OEMWriter - Class in org.orekit.files.ccsds

An OEM Writer class that can take in a general EphemerisFile object and export it as a valid OEM file.

OEMWriter() - Constructor for class org.orekit.files.ccsds.OEMWriter

Standard default constructor that creates a writer with default configurations.

OEMWriter(OEMWriter.InterpolationMethod, String, String, String) - Constructor for class org.orekit.files.ccsds.OEMWriter

Constructor used to create a new OEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard @{link EphemerisFile} object.

OEMWriter.InterpolationMethod - Enum in org.orekit.files.ccsds

OEM interpolation method.

OFFSET_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation

Suffix for ground station position and clock offset parameters names.

offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Compute the apparent clock offset between two instant in the perspective of a specific time scale.

offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents

Compute the seconds offset between two instances.

offsetFrom(FieldAbsoluteDate<T>, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Compute the apparent clock offset between two instant in the perspective of a specific time scale.

offsetFromBoundary(Vector3D) - Method in class org.orekit.propagation.events.FieldOfView

Get the angular offset of target point with respect to the Field Of View Boundary.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.BDTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GalileoScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GMSTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GPSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.IRNSSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.QZSSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TAIScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UT1Scale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.BDTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GalileoScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GMSTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GPSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.IRNSSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.QZSSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TAIScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCGScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TDBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UT1Scale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale

Get the offset to convert locations from TAIScale to instance.

OffsetModel - Class in org.orekit.time

TAI UTC offset model.

OffsetModel(DateComponents, int) - Constructor for class org.orekit.time.OffsetModel

Constructor for a constant offset model.

OffsetModel(DateComponents, int, double, double) - Constructor for class org.orekit.time.OffsetModel

Constructor for a linear offset model.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.BDTScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GalileoScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GLONASSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GPSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.IRNSSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.QZSSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TAIScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TTScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale

Get the offset to convert locations from instance to TAIScale.

OGMFile - Class in org.orekit.files.ccsds

This class gathers the general state data present in both OPM and OMM files.

omega - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final perigee argument.

omgdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for perigee argument (omega) computation.

OMMFile - Class in org.orekit.files.ccsds

This class gathers the informations present in the Orbital Mean-Elements Message (OMM), and contains methods to generate a CartesianOrbit, a KeplerianOrbit, a SpacecraftState and, eventually, a TLE.

OMMFile.OMMMetaData - Class in org.orekit.files.ccsds

OMMParser - Class in org.orekit.files.ccsds

A parser for the CCSDS OMM (Orbiter Mean-Elements Message).

OMMParser() - Constructor for class org.orekit.files.ccsds.OMMParser

Simple constructor.

OnBoardAntennaInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers

On-board antenna offset effect on inter-satellites range measurements.

OnBoardAntennaInterSatellitesRangeModifier(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier

Simple constructor.

OnBoardAntennaRangeModifier - Class in org.orekit.estimation.measurements.modifiers

On-board antenna offset effect on range measurements.

OnBoardAntennaRangeModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier

Simple constructor.

OnBoardAntennaTurnAroundRangeModifier - Class in org.orekit.estimation.measurements.modifiers

On-board antenna offset effect on turn around range measurements.

OnBoardAntennaTurnAroundRangeModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier

Simple constructor.

onDate(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the normalized spherical harmonic coefficients at a specific instance in time.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider

Get the normalized spherical harmonic coefficients at a specific instance in time.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider

Get the raw spherical harmonic coefficients on a specific date.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider

Get the un-normalized spherical harmonic coefficients at a specific instance in time.

ONE - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

1 represented as a polynomial.

OneAxisEllipsoid - Class in org.orekit.bodies

Modeling of a one-axis ellipsoid.

OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid

Simple constructor.

ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

1 / A .

ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

1 / (A * B) .

ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

1 / (1 + B) .

ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

1 / μ .

openStream() - Method in interface org.orekit.data.NamedData.StreamOpener

Open the stream.

OPMFile - Class in org.orekit.files.ccsds

This class gathers the informations present in the Orbital Parameter Message (OPM), and contains methods to generate CartesianOrbit, KeplerianOrbit or SpacecraftState.

OPMFile.Maneuver - Class in org.orekit.files.ccsds

Maneuver in an OPM file.

OPMParser - Class in org.orekit.files.ccsds

A parser for the CCSDS OPM (Orbit Parameter Message).

OPMParser() - Constructor for class org.orekit.files.ccsds.OPMParser

Simple constructor.

Orbit - Class in org.orekit.orbits

This class handles orbital parameters.

Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit

Default constructor.

Orbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.Orbit

Set the orbit from Cartesian parameters.

ORBIT_A_E_MISMATCH_WITH_CONIC_TYPE - org.orekit.errors.OrekitMessages

ORBIT_AND_ATTITUDE_DATES_MISMATCH - org.orekit.errors.OrekitMessages

ORBIT_ANOMALY_OUT_OF_HYPERBOLIC_RANGE - org.orekit.errors.OrekitMessages

ORBIT_TYPE_NOT_ALLOWED - org.orekit.errors.OrekitMessages

OrbitType - Enum in org.orekit.orbits

Enumerate for orbital parameters types.

orCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that is the logical OR or the given event detectors.

orCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that is the logical OR or the given event detectors.

OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager

Name of the property defining the root directories or zip/jar files path for default configuration.

OrekitConfiguration - Class in org.orekit.utils

Utility class for setting global configuration parameters.

OrekitEphemerisFile - Class in org.orekit.files.general

A class for encapsulating Orekit propagators within an EphemerisFile complaint object that makes for easy serialization to external ephemeris formats like OEM.

OrekitEphemerisFile() - Constructor for class org.orekit.files.general.OrekitEphemerisFile

Standard default constructor.

OrekitEphemerisFile.OrekitEphemerisSegment - Class in org.orekit.files.general

OrekitEphemerisFile.OrekitSatelliteEphemeris - Class in org.orekit.files.general

Inner class of OrekitEphemerisFile that defines the OrekitEphemerisFile.OrekitSatelliteEphemeris corresponding object for this ephemeris type.

OrekitEphemerisSegment(List<TimeStampedPVCoordinates>, Frame, String, double, TimeScale, int) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

constructor for OrekitEphemerisSegment.

OrekitException - Exception in org.orekit.errors

This class is the base class for all specific exceptions thrown by the Orekit classes.

OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(MathRuntimeException) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException

Copy constructor.

OrekitExceptionWrapper - Exception in org.orekit.errors

Deprecated.

as of 9.3, this class is not used anymore, as OrekitException is now an unchecked exception

OrekitExceptionWrapper(OrekitException) - Constructor for exception org.orekit.errors.OrekitExceptionWrapper

Deprecated.

Simple constructor.

OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware fixed size step handler.

OrekitIllegalArgumentException - Exception in org.orekit.errors

Extension of IllegalArgumentException with localized message.

OrekitIllegalArgumentException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalArgumentException

Create an exception with localized message.

OrekitIllegalStateException - Exception in org.orekit.errors

Extension of IllegalStateException with localized message.

OrekitIllegalStateException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalStateException

Create an exception with localized message.

OrekitInternalError - Exception in org.orekit.errors

Extension of Runtime with localized message for internal errors only.

OrekitInternalError(Throwable) - Constructor for exception org.orekit.errors.OrekitInternalError

Create an exception with localized message.

OrekitIOException - Exception in org.orekit.errors

Extension of IOException with localized message.

OrekitIOException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIOException

Create an exception with localized message.

OrekitMessages - Enum in org.orekit.errors

Enumeration for localized messages formats.

OrekitMessages.UTF8Control - Class in org.orekit.errors

Control class loading properties in UTF-8 encoding.

OrekitParseException - Exception in org.orekit.errors

Extension of ParseException with localized message.

OrekitParseException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitParseException

Create an exception with localized message.

OrekitSatelliteEphemeris(String) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Standard constructor for building the satellite Ephemeris object.

OrekitStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step handler.

OrekitStepHandlerMultiplexer - Class in org.orekit.propagation.sampling

This class gathers several OrekitStepHandler instances into one.

OrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer

Simple constructor.

OrekitStepInterpolator - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step interpolator.

OrekitStepNormalizer - Class in org.orekit.propagation.sampling

This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.

OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer

Simple constructor.

org.orekit.attitudes - package org.orekit.attitudes

This package provides classes to represent simple attitudes.

org.orekit.bodies - package org.orekit.bodies

This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.

org.orekit.data - package org.orekit.data

This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.

org.orekit.errors - package org.orekit.errors

This package provides classes to generate and handle exceptions.

org.orekit.estimation - package org.orekit.estimation

This package is the top level package for orbit determination.

org.orekit.estimation.iod - package org.orekit.estimation.iod

org.orekit.estimation.leastsquares - package org.orekit.estimation.leastsquares

The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.

org.orekit.estimation.measurements - package org.orekit.estimation.measurements

The measurements package defines everything that is related to orbit determination measurements.

org.orekit.estimation.measurements.generation - package org.orekit.estimation.measurements.generation

This package provides Orbit Determination measurements generation.

org.orekit.estimation.measurements.modifiers - package org.orekit.estimation.measurements.modifiers

org.orekit.estimation.sequential - package org.orekit.estimation.sequential

org.orekit.files - package org.orekit.files

Top level package for various parsers.

org.orekit.files.ccsds - package org.orekit.files.ccsds

This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.

org.orekit.files.general - package org.orekit.files.general

This package provides interfaces for orbit file representations and corresponding parsers.

org.orekit.files.sp3 - package org.orekit.files.sp3

This package provides a parser for orbit data stored in SP3 format.

org.orekit.forces - package org.orekit.forces

This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).

org.orekit.forces.drag - package org.orekit.forces.drag

This package provides all drag-related forces.

org.orekit.forces.drag.atmosphere - package org.orekit.forces.drag.atmosphere

This package provides the atmosphere model interface and several implementations.

org.orekit.forces.drag.atmosphere.data - package org.orekit.forces.drag.atmosphere.data

This package provides classes to get atmospheric data, including solar flux and planetary geomagnetic indices.

org.orekit.forces.gravity - package org.orekit.forces.gravity

This package provides all gravity-related forces.

org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential

This package provides classes to read gravity field files and supports several different formats.

org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers

This package provides models of simple maneuvers.

org.orekit.forces.radiation - package org.orekit.forces.radiation

This package provides all radiation pressure related forces.

org.orekit.frames - package org.orekit.frames

This package provides classes to handle frames and transforms between them.

org.orekit.gnss - package org.orekit.gnss

This package provides classes related to GNSS applications.

org.orekit.gnss.antenna - package org.orekit.gnss.antenna

This package provides classes related to receiver and satellites antenna modeling.

org.orekit.gnss.attitude - package org.orekit.gnss.attitude

This package provides classes related to navigation satellites attitude modeling.

org.orekit.models - package org.orekit.models

Top level package for physical models.

org.orekit.models.earth - package org.orekit.models.earth

This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.

org.orekit.models.earth.displacement - package org.orekit.models.earth.displacement

This package provides models computing reference points displacements on Earth surface.

org.orekit.models.earth.tessellation - package org.orekit.models.earth.tessellation

This package provides ways to do tessellation and sampling of zones of interest over an ellipsoid surface.

org.orekit.orbits - package org.orekit.orbits

This package provides classes to represent orbits.

org.orekit.propagation - package org.orekit.propagation

Propagation

org.orekit.propagation.analytical - package org.orekit.propagation.analytical

Top level package for analytical propagators.

org.orekit.propagation.analytical.gnss - package org.orekit.propagation.analytical.gnss

This package provides classes to propagate GNSS orbits.

org.orekit.propagation.analytical.tle - package org.orekit.propagation.analytical.tle

This package provides classes to read and extrapolate tle's.

org.orekit.propagation.conversion - package org.orekit.propagation.conversion

This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.

org.orekit.propagation.events - package org.orekit.propagation.events

This package provides interfaces and classes dealing with events occurring during propagation.

org.orekit.propagation.events.handlers - package org.orekit.propagation.events.handlers

This package provides an interface and classes dealing with events occurrence only.

org.orekit.propagation.integration - package org.orekit.propagation.integration

Utilities for integration-based propagators (both numerical and semi-analytical).

org.orekit.propagation.numerical - package org.orekit.propagation.numerical

Top level package for numerical propagators.

org.orekit.propagation.sampling - package org.orekit.propagation.sampling

This package provides interfaces and classes dealing with step handling during propagation.

org.orekit.propagation.semianalytical - package org.orekit.propagation.semianalytical

Top level package for semi-analytical propagators.

org.orekit.propagation.semianalytical.dsst - package org.orekit.propagation.semianalytical.dsst

This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

org.orekit.propagation.semianalytical.dsst.forces - package org.orekit.propagation.semianalytical.dsst.forces

This package provides force models for Draper Semi-analytical Satellite Theory (DSST).

org.orekit.propagation.semianalytical.dsst.utilities - package org.orekit.propagation.semianalytical.dsst.utilities

This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).

org.orekit.propagation.semianalytical.dsst.utilities.hansen - package org.orekit.propagation.semianalytical.dsst.utilities.hansen

This package provides Hansen coefficient related utilities for Draper Semi-analytical Satellite Theory (DSST).

org.orekit.time - package org.orekit.time

This independent package provides classes to handle epochs, time scales, and to compare instants together.

org.orekit.utils - package org.orekit.utils

This package provides useful objects.

ORIGINATOR - org.orekit.files.ccsds.Keyword

Creating agency or operator.

OrphanFrame - Class in org.orekit.frames

Prototype frame that can be built from leaf to roots and later attached to a tree.

OrphanFrame(String) - Constructor for class org.orekit.frames.OrphanFrame

Simple constructor.

osculatingDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating derivative.

osculatingSecondDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating second derivative.

OsculatingToMeanElementsConverter - Class in org.orekit.propagation.conversion

This class converts osculating orbital elements into mean elements.

OsculatingToMeanElementsConverter(SpacecraftState, int, Propagator, double) - Constructor for class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter

Constructor.

osculatingValue(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating value.

OTHER - org.orekit.files.sp3.SP3File.SP3OrbitType

other type, defined by SP3 file producing agency.

OUT_OF_RANGE_BODY_EPHEMERIDES_DATE - org.orekit.errors.OrekitMessages

OUT_OF_RANGE_DERIVATION_ORDER - org.orekit.errors.OrekitMessages

OUT_OF_RANGE_EPHEMERIDES_DATE - org.orekit.errors.OrekitMessages

OUT_OF_RANGE_LATITUDE - org.orekit.errors.OrekitMessages

OUT_OF_RANGE_SECONDS_NUMBER - org.orekit.errors.OrekitMessages

OUT_OF_RANGE_TIME_TRANSFORM - org.orekit.errors.OrekitMessages

OutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers

Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.

OutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OutlierFilter

Simple constructor.

P

p - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

h_y.

P1 - org.orekit.gnss.ObservationType

Pseudorange GPS L1 / GLONASS G1 for Rinex2.

P1 - Static variable in class org.orekit.models.earth.displacement.Tide

P₁ tide.

P2 - org.orekit.gnss.ObservationType

Pseudorange GPS L2 / GLONASS G2 for Rinex2.

ParameterDriver - Class in org.orekit.utils

Class allowing to drive the value of a parameter.

ParameterDriver(String, double, double, double, double) - Constructor for class org.orekit.utils.ParameterDriver

Simple constructor.

ParameterDriversList - Class in org.orekit.utils

Class managing several parameter drivers, taking care of duplicated names.

ParameterDriversList() - Constructor for class org.orekit.utils.ParameterDriversList

Creates an empty list.

ParameterDriversList.DelegatingDriver - Class in org.orekit.utils

Specialized driver delegating to several other managing the same parameter name.

ParameterFunction - Interface in org.orekit.utils

Interface representing a scalar function depending on a ParameterDriver.

ParameterObserver - Interface in org.orekit.utils

Interface for observing parameters changes.

parse(BufferedReader, String) - Method in class org.orekit.files.ccsds.OEMParser

parse(BufferedReader, String) - Method in interface org.orekit.files.general.EphemerisFileParser

Parse an ephemeris file from a stream.

parse(BufferedReader, String) - Method in class org.orekit.files.sp3.SP3Parser

parse(InputStream) - Method in class org.orekit.files.ccsds.ODMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream) - Method in class org.orekit.files.ccsds.OEMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream) - Method in class org.orekit.files.ccsds.OMMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream) - Method in class org.orekit.files.ccsds.OPMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream) - Method in class org.orekit.files.ccsds.TDMParser

Parse a CCSDS Tracking Data Message.

parse(InputStream) - Method in class org.orekit.files.sp3.SP3Parser

Parse a SP3 file from an input stream using the UTF-8 charset.

parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser

Parse a stream.

parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser

Parse a stream.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.ODMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.OEMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.OMMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.OPMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.TDMParser

Parse a CCSDS Tracking Data Message.

parse(String) - Method in class org.orekit.data.PolynomialParser

Parse a polynomial expression.

parse(String) - Method in class org.orekit.files.ccsds.ODMParser

Parse a CCSDS Orbit Data Message.

parse(String) - Method in class org.orekit.files.ccsds.OEMParser

Parse a CCSDS Orbit Data Message.

parse(String) - Method in class org.orekit.files.ccsds.OMMParser

Parse a CCSDS Orbit Data Message.

parse(String) - Method in class org.orekit.files.ccsds.OPMParser

Parse a CCSDS Orbit Data Message.

parse(String) - Method in class org.orekit.files.ccsds.TDMParser

Parse a CCSDS Tracking Data Message.

parse(String) - Method in interface org.orekit.files.general.EphemerisFileParser

Parse an ephemeris file from a file on the local file system.

parse(String) - Method in class org.orekit.files.sp3.SP3Parser

parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Calendar Segmented Time Code (CCS).

parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Calendar Segmented Time Code (CCS).

parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Day Segmented Time Code (CDS).

parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Day Segmented Time Code (CDS).

parseCCSDSFrame(String) - Method in class org.orekit.files.ccsds.ODMParser

Parse a CCSDS frame.

parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Unsegmented Time Code (CUC).

parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Unsegmented Time Code (CUC).

parseCoefficient(String, double[][], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Parse a coefficient.

parseCoefficient(String, List<List<Double>>, int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Parse a coefficient.

parseComment(KeyValue, List<String>) - Method in class org.orekit.files.ccsds.ODMParser

Parse a comment line.

parseDate(String) - Static method in class org.orekit.time.DateComponents

Parse a string in ISO-8601 format to build a date.

parseDate(String, CcsdsTimeScale) - Method in class org.orekit.files.ccsds.ODMParser

Parse a date.

parseDate(String, IERSConventions, AbsoluteDate) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale

Parse a date in this time scale.

parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents

Parse a string in ISO-8601 format to build a date/time.

parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Parse a double from a string.

parseGeneralStateDataEntry(KeyValue, OGMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser

Parse a general state data key = value entry.

parseHeaderEntry(KeyValue, ODMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser

Parse an entry from the header.

parseKeyValue(InputStream, String) - Method in class org.orekit.files.ccsds.TDMParser

Parse a CCSDS Tracking Data Message with KEYVALUE format.

parseMetaDataEntry(KeyValue, ODMMetaData, List<String>) - Method in class org.orekit.files.ccsds.ODMParser

Parse a meta-data key = value entry.

parseMonth(String) - Static method in enum org.orekit.time.Month

Parse the string to get the month.

Parser() - Constructor for class org.orekit.gnss.RinexLoader.Parser

parseSatelliteAntennaCode(String) - Static method in enum org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

Parse a string to get the satellite antenna code.

parseSatelliteSystem(String) - Static method in enum org.orekit.gnss.SatelliteSystem

Parse a string to get the satellite system.

parseSatelliteType(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType

Parse a string to get the satellite type.

parseTime(String) - Static method in class org.orekit.time.TimeComponents

Parse a string in ISO-8601 format to build a time.

parseType(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType

Parse a string to get the type.

parseXml(InputStream, String) - Method in class org.orekit.files.ccsds.TDMParser

Parse a CCSDS Tracking Data Message with XML format.

PartialDerivativesEquations - Class in org.orekit.propagation.numerical

Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.

PartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.PartialDerivativesEquations

Simple constructor.

PARTICIPANT_1 - org.orekit.files.ccsds.Keyword

Meta-data: PARTICIPANT_n, n = {1, 2, 3, 4, 5}.

PARTICIPANT_2 - org.orekit.files.ccsds.Keyword

Participant 2.

PARTICIPANT_3 - org.orekit.files.ccsds.Keyword

Participant 3.

PARTICIPANT_4 - org.orekit.files.ccsds.Keyword

Participant 4.

PARTICIPANT_5 - org.orekit.files.ccsds.Keyword

Participant 5.

PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate

Dummy date at infinity in the past direction.

PATH - org.orekit.files.ccsds.Keyword

Meta-data: The PATH keywords shall reflect the signal path by listing the index of each PARTICIPANT in order, separated by commas, with no inserted white space.

PATH_1 - org.orekit.files.ccsds.Keyword

Path 1.

PATH_2 - org.orekit.files.ccsds.Keyword

Path 2.

pathDelay(double, double) - Method in class org.orekit.models.earth.FixedTroposphericDelay

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, double) - Method in class org.orekit.models.earth.MariniMurrayModel

pathDelay(double, double) - Method in class org.orekit.models.earth.SaastamoinenModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, double) - Method in interface org.orekit.models.earth.TroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.DiscreteTroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.EstimatedTroposphericModel

pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.MendesPavlisModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.TroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaOneModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaThreeModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(AbsoluteDate, GeodeticPoint, double, double) - Method in interface org.orekit.models.earth.IonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(AbsoluteDate, GeodeticPoint, double, double) - Method in class org.orekit.models.earth.KlobucharIonoModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, T) - Method in interface org.orekit.models.earth.TroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.DiscreteTroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.EstimatedTroposphericModel

pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.MendesPavlisModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.TroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaOneModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaThreeModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

PC_N0 - org.orekit.files.ccsds.Keyword

Data: Carrier power to noise spectral density ratio (Pc/No) [dBHz].

perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

perigee, expressed in KM and ALTITUDE.

Phase - Class in org.orekit.estimation.measurements

Class modeling a phase measurement from a ground station.

Phase(GroundStation, AbsoluteDate, double, double, double, double) - Constructor for class org.orekit.estimation.measurements.Phase

Deprecated.

since 9.3 raplced by Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite)

Phase(GroundStation, AbsoluteDate, double, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.Phase

Deprecated.

since 9.3 raplced by Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite)

Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Phase

Simple constructor.

PhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical phase measurement with ambiguity.

PhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier

Constructor.

PhaseCenterVariationFunction - Interface in org.orekit.gnss.antenna

Model for antennas phase center variations.

PLUTO - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for Pluto.

PLUTO - org.orekit.files.ccsds.CenterName

Pluto body.

PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Pluto.

POINT_INSIDE_ELLIPSOID - org.orekit.errors.OrekitMessages

pointAt(double) - Method in class org.orekit.bodies.Ellipse

Get a point of the 2D ellipse.

pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame

Compute the point observed from the station at some specified distance.

pointOnLimb(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid

Find a point on ellipsoid limb, as seen by an external observer.

PoissonSeries - Class in org.orekit.data

Class representing a Poisson series for nutation or ephemeris computations.

PoissonSeries(PolynomialNutation, Map<Long, SeriesTerm>) - Constructor for class org.orekit.data.PoissonSeries

Build a Poisson series from an IERS table file.

PoissonSeries.CompiledSeries - Interface in org.orekit.data

This interface represents a fast evaluator for Poisson series.

PoissonSeriesParser - Class in org.orekit.data

Parser for Poisson series files.

PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser

Build a parser for a Poisson series from an IERS table file.

POLAR_TRAJECTORY - org.orekit.errors.OrekitMessages

PoleCorrection - Class in org.orekit.frames

Simple container class for pole correction parameters.

PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection

Simple constructor.

PolynomialFunctionMatrix - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

A quadratic matrix of PolynomialFunction.

PolynomialNutation - Class in org.orekit.data

Polynomial nutation function.

PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation

Build a polynomial from its coefficients.

PolynomialParametricAcceleration - Class in org.orekit.forces

This class implements a parametric acceleration with polynomial signed amplitude.

PolynomialParametricAcceleration(Vector3D, boolean, String, AbsoluteDate, int) - Constructor for class org.orekit.forces.PolynomialParametricAcceleration

Simple constructor.

PolynomialParametricAcceleration(Vector3D, AttitudeProvider, String, AbsoluteDate, int) - Constructor for class org.orekit.forces.PolynomialParametricAcceleration

Simple constructor.

PolynomialParser - Class in org.orekit.data

Parser for polynomials in IERS tables.

PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser

Simple constructor.

PolynomialParser.Unit - Enum in org.orekit.data

Unit for the coefficients.

Position - Class in org.orekit.estimation.measurements

Class modeling a position only measurement.

Position(AbsoluteDate, Vector3D, double[][], double) - Constructor for class org.orekit.estimation.measurements.Position

Deprecated.

as of 9.3, replaced by Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite)

Position(AbsoluteDate, Vector3D, double[][], double, int) - Constructor for class org.orekit.estimation.measurements.Position

Deprecated.

as of 9.3, replaced by Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite)

Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position

Constructor with full covariance matrix and all inputs.

Position(AbsoluteDate, Vector3D, double[], double) - Constructor for class org.orekit.estimation.measurements.Position

Deprecated.

as of 9.3, replaced by Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite)

Position(AbsoluteDate, Vector3D, double[], double, int) - Constructor for class org.orekit.estimation.measurements.Position

Deprecated.

as of 9.3, replaced by Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite)

Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position

Constructor with one vector for the standard deviation.

Position(AbsoluteDate, Vector3D, double, double) - Constructor for class org.orekit.estimation.measurements.Position

Deprecated.

as of 9.3, replaced by Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite)

Position(AbsoluteDate, Vector3D, double, double, int) - Constructor for class org.orekit.estimation.measurements.Position

Deprecated.

as of 9.3, replaced by Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite)

Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position

Constructor with one double for the standard deviation.

PositionAngle - Enum in org.orekit.orbits

Enumerate for true, eccentric and mean position angles.

PositionAngleDetector - Class in org.orekit.propagation.events

Detector for in-orbit position angle.

PositionAngleDetector(double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector

Build a detector.

PositionAngleDetector(OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector

Build a new detector.

PositionBuilder - Class in org.orekit.estimation.measurements.generation

Builder for Position measurements.

PositionBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PositionBuilder

Simple constructor.

POSITIVE_FLOW_RATE - org.orekit.errors.OrekitMessages

PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential

This abstract class represents a Gravitational Potential Coefficients file reader.

PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Simple constructor.

PR_N0 - org.orekit.files.ccsds.Keyword

Data: Ranging power to noise spectral density ratio (Pr/No) [dBHz].

Predefined - Enum in org.orekit.frames

Predefined frames provided by FramesFactory.

PRESSURE - org.orekit.files.ccsds.Keyword

Data: Pressure [hPa].

PROCESSED - org.orekit.estimation.measurements.EstimatedMeasurement.Status

Status for processed measurements.

processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.KalmanEstimator

Process several measurements.

projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse

Find the closest ellipse point.

projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse

Project position-velocity-acceleration on an ellipse.

projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape

Project a point to the ground.

projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid

Project a point to the ground.

projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.models.earth.Geoid

projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape

Project a moving point to the ground.

projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid

Project a moving point to the ground.

projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.models.earth.Geoid

propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator

Propagate towards a target date.

propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Propagate towards a target date.

propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator

Propagate towards a target date.

propagate(AbsoluteDate, boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Propagation with or without event detection.

propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Propagate from a start date towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Propagate from a start date towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator

Propagate from a start date towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.PropagatorsParallelizer

Propagate from a start date towards a target date.

propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Propagate towards a target date.

propagate(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator

Propagate towards a target date.

propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Propagate towards a target date.

propagate(FieldAbsoluteDate<T>, boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Propagation with or without event detection.

propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Propagate from a start date towards a target date.

propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator

Propagate from a start date towards a target date.

propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Propagate from a start date towards a target date.

propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Gets the PVCoordinates of the GPS SV in ECEF frame.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Extrapolate an orbit up to a specific target date.

Propagator - Interface in org.orekit.propagation

This interface provides a way to propagate an orbit at any time.

PROPAGATOR_NOT_IN_EPHEMERIS_GENERATION_MODE - org.orekit.errors.OrekitMessages

PropagatorBuilder - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction to build propagators for conversion.

PropagatorConverter - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction for propagators conversions.

PropagatorsParallelizer - Class in org.orekit.propagation

This class provides a way to propagate simultaneously several orbits.

PropagatorsParallelizer(List<Propagator>, MultiSatStepHandler) - Constructor for class org.orekit.propagation.PropagatorsParallelizer

Simple constructor.

PSEUDO_RANGE - org.orekit.gnss.MeasurementType

Pseudo-range measurement.

PV - Class in org.orekit.estimation.measurements

Class modeling a position-velocity measurement.

PV(AbsoluteDate, Vector3D, Vector3D, double[][], double) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, int) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with 2 smaller covariance matrices.

PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, int) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with full covariance matrix and all inputs.

PV(AbsoluteDate, Vector3D, Vector3D, double[], double) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, int) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with two vectors for the standard deviations.

PV(AbsoluteDate, Vector3D, Vector3D, double[], double, int) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with one vector for the standard deviations.

PV(AbsoluteDate, Vector3D, Vector3D, double, double, double) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.PV

Deprecated.

as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite)

PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with two double for the standard deviations.

PVBuilder - Class in org.orekit.estimation.measurements.generation

Builder for PV measurements.

PVBuilder(CorrelatedRandomVectorGenerator, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PVBuilder

Simple constructor.

PVCoordinates - Class in org.orekit.utils

Simple container for Position/Velocity/Acceleration triplets.

PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates

Simple constructor.

PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Multiplicative constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet from a FieldVector3D<DerivativeStructure>.

PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet with zero acceleration.

PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet.

PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Subtractive constructor.

PVCoordinatesProvider - Interface in org.orekit.utils

Interface for PV coordinates providers.

Q

q - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

h_x.

Q1 - Static variable in class org.orekit.models.earth.displacement.Tide

Q₁ tide.

QSW - org.orekit.frames.LOFType

Constant for QSW frame (X axis aligned with position, Z axis aligned with orbital momentum).

QZS - org.orekit.files.sp3.SP3File.TimeSystem

Quasi-Zenith System.

QZSS - org.orekit.files.sp3.SP3File.SP3FileType

QZSS only file.

QZSS - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

QZSS Block I (Michibiki-1).

QZSS - org.orekit.gnss.antenna.SatelliteType

QZSS Block I (Michibiki-1).

QZSS - org.orekit.gnss.SatelliteSystem

Quasi-Zenith Satellite System system.

QZSS_2G - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

QZSS Block II GEO (Michibiki-3).

QZSS_2G - org.orekit.gnss.antenna.SatelliteType

QZSS Block II GEO (Michibiki-3).

QZSS_2I - org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

QZSS Block II IGSO (Michibiki-2,4).

QZSS_2I - org.orekit.gnss.antenna.SatelliteType

QZSS Block II IGSO (Michibiki-2,4).

QZSSScale - Class in org.orekit.time

QZSS time scale.

R

R01 - org.orekit.gnss.Frequency

GLONASS, "G1" (1602 MHZ).

R02 - org.orekit.gnss.Frequency

GLONASS, "G2" (1246 MHz).

R03 - org.orekit.gnss.Frequency

GLONASS, "G3" (1202.025 MHz).

RA_OF_ASC_NODE - org.orekit.files.ccsds.Keyword

Orbit right ascension of ascending node.

RADIANS - org.orekit.data.PolynomialParser.Unit

Radians angles.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to radiation pressure, with parameters derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Compute the acceleration due to radiation pressure, with parameters derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Compute the acceleration due to radiation pressure, with parameters derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Compute the acceleration due to radiation pressure, with parameters derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Compute the acceleration due to radiation pressure, with parameters derivatives.

radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Compute the acceleration due to radiation pressure.

RadiationSensitive - Interface in org.orekit.forces.radiation

Interface for spacecraft that are sensitive to radiation pressure forces.

Range - Class in org.orekit.estimation.measurements

Class modeling a range measurement from a ground station.

Range(GroundStation, boolean, AbsoluteDate, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.Range

Deprecated.

as of 9.3, replaced by Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite)

Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Range

Simple constructor.

Range(GroundStation, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.Range

Deprecated.

as of 9.3, replaced by Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite)

Range(GroundStation, AbsoluteDate, double, double, double, boolean) - Constructor for class org.orekit.estimation.measurements.Range

Deprecated.

as of 9.3, replaced by Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite)

Range(GroundStation, AbsoluteDate, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.Range

Deprecated.

as of 9.3, replaced by Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite)

RANGE - org.orekit.files.ccsds.Keyword

Data: Range value [km, s or RU].

RANGE_MODE - org.orekit.files.ccsds.Keyword

Meta-data: Range mode.

RANGE_MODULUS - org.orekit.files.ccsds.Keyword

Meta-data: Range modulus.

RANGE_UNITS - org.orekit.files.ccsds.Keyword

Meta-data: The RANGE_UNITS keyword specifies the units for the range observable.

RangeBuilder - Class in org.orekit.estimation.measurements.generation

Builder for Range measurements.

RangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeBuilder

Simple constructor.

RangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with ionospheric delay.

RangeIonosphericDelayModifier(IonosphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier

Constructor.

RangeRate - Class in org.orekit.estimation.measurements

Class modeling one-way or two-way range rate measurement between two vehicles.

RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean) - Constructor for class org.orekit.estimation.measurements.RangeRate

Deprecated.

since 9.3 replaced by RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite)

RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, int) - Constructor for class org.orekit.estimation.measurements.RangeRate

Deprecated.

since 9.3 replaced by RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite)

RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.RangeRate

Simple constructor.

RangeRateBuilder - Class in org.orekit.estimation.measurements.generation

Builder for RangeRate measurements.

RangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeRateBuilder

Simple constructor.

rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Compute the measurement error due to Troposphere.

rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Compute the measurement error due to Troposphere.

RangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range-rate measurement with ionospheric delay.

RangeRateIonosphericDelayModifier(IonosphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier

Constructor.

RangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range-rate measurements with tropospheric delay.

RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Constructor.

RangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with tropospheric delay.

RangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier

Constructor.

RAPID_DATA_PREDICITON_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).

RAPID_DATA_PREDICITON_XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP XML files (IAU2000 compatibles).

RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).

RAPID_DATA_PREDICTION_XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP XML files (IAU1980 compatibles).

RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide raw spherical harmonics coefficients.

RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

The raw spherical harmonics at a particular instant.

readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Read a gravity field coefficients provider from the first supported file.

rebuildZone() - Method in class org.orekit.utils.SphericalPolygonsSetTransferObject

Rebuild the zone from saved data.

RECEIVE_BAND - org.orekit.files.ccsds.Keyword

Meta-data: Frequency band for received frequencies.

RECEIVE_DELAY_1 - org.orekit.files.ccsds.Keyword

Meta-data: Receive delays list.

RECEIVE_DELAY_2 - org.orekit.files.ccsds.Keyword

Second.

RECEIVE_DELAY_3 - org.orekit.files.ccsds.Keyword

Second.

RECEIVE_DELAY_4 - org.orekit.files.ccsds.Keyword

Second.

RECEIVE_DELAY_5 - org.orekit.files.ccsds.Keyword

Second.

RECEIVE_FREQ - org.orekit.files.ccsds.Keyword

Data: Received frequency [Hz].

RECEIVE_FREQ_1 - org.orekit.files.ccsds.Keyword

Data: Received frequencies [Hz].

RECEIVE_FREQ_2 - org.orekit.files.ccsds.Keyword

Received frequency 2.

RECEIVE_FREQ_3 - org.orekit.files.ccsds.Keyword

Received frequency 3.

RECEIVE_FREQ_4 - org.orekit.files.ccsds.Keyword

Received frequency 4.

RECEIVE_FREQ_5 - org.orekit.files.ccsds.Keyword

Received frequency 5.

ReceiverAntenna - Class in org.orekit.gnss.antenna

GNSS receiver antenna model.

ReceiverAntenna(String, String, Map<Frequency, FrequencyPattern>, String) - Constructor for class org.orekit.gnss.antenna.ReceiverAntenna

Simple constructor.

RecordAndContinue<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Handler that will record every time an event occurs and always return EventHandler.Action.CONTINUE.

RecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue

Create a new handler using an ArrayList to store events.

RecordAndContinue(List<RecordAndContinue.Event<T>>) - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue

Create a handler using the given collection to store events.

RecordAndContinue.Event<T> - Class in org.orekit.propagation.events.handlers

A single event detected during propagation.

REF_FRAME - org.orekit.files.ccsds.Keyword

Name of the reference frame in which the state vector and optional Keplerian element data are given.

REF_FRAME_EPOCH - org.orekit.files.ccsds.Keyword

Epoch of reference frame, if not intrinsic to the definition of the reference frame.

REFERENCE_FRAME - org.orekit.files.ccsds.Keyword

Reference frame in which data are given: used in combination with ANGLE_TYPE=RADEC.

referenceDateChanged(AbsoluteDate, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter reference date has been changed.

ReferenceEllipsoid - Class in org.orekit.models.earth

A Reference Ellipsoid for use in geodesy.

ReferenceEllipsoid(double, double, Frame, double, double) - Constructor for class org.orekit.models.earth.ReferenceEllipsoid

Creates a new geodetic Reference Ellipsoid from four defining parameters.

referenceValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter reference value has been changed.

REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive

Parameter name for reflection coefficient.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Register an attitude provider.

registerSwitchEvents(Field<T>, FieldPropagator<T>) - Method in class org.orekit.attitudes.AttitudesSequence

Register all wrapped switch events to the propagator.

registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence

Register all wrapped switch events to the propagator.

reinitializeBegin(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState

Reinitialize the beginning of the step.

reinitializeBegin(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState

Reinitialize the beginning of the step.

REJECTED - org.orekit.estimation.measurements.EstimatedMeasurement.Status

Status for rejected measurements.

Relativity - Class in org.orekit.forces.gravity

Post-Newtonian correction force due to general relativity.

Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity

Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.

removeForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Remove all perturbing force models from the global perturbation model.

removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Remove all force models (except central attraction).

removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Remove all perturbing force models from the global perturbation model.

removeObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver

Remove an observer.

removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Remove one provider.

requiresDenseOutput() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Determines whether this handler needs dense output.

requiresDenseOutput() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Determines whether this handler needs dense output.

rescale(double, boolean, double[][], double[][], boolean, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Rescale coefficients arrays.

RESET_DERIVATIVES - org.orekit.propagation.events.handlers.EventHandler.Action

Reset derivatives indicator.

RESET_DERIVATIVES - org.orekit.propagation.events.handlers.FieldEventHandler.Action

Reset derivatives indicator.

RESET_STATE - org.orekit.propagation.events.handlers.EventHandler.Action

Reset state indicator.

RESET_STATE - org.orekit.propagation.events.handlers.FieldEventHandler.Action

Reset state indicator.

resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence

Reset the active provider.

resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic

Reset fitting.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris

Try (and fail) to reset the initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Reset the initial state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.Ephemeris

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Reset an intermediate state.

resetOrbit(Orbit) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Reset the orbit in the propagator builder.

resetState(KK, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler

Reset the state prior to continue propagation.

resetState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Reset the state prior to continue propagation.

resetState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector

Reset the state prior to continue propagation.

resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector

Reset the state prior to continue propagation.

resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector

Reset the state prior to continue propagation.

resetState(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector

Reset the state prior to continue propagation.

resetState(T, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler

Reset the state prior to continue propagation.

resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue

restrictStep(SpacecraftState, SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Create a new restricted version of the instance.

REV_AT_EPOCH - org.orekit.files.ccsds.Keyword

Revolution Number.

revert() - Method in class org.orekit.utils.AngularCoordinates

Revert a rotation/rotation rate/ rotation acceleration triplet.

revert() - Method in class org.orekit.utils.FieldAngularCoordinates

Revert a rotation / rotation rate / rotation acceleration triplet.

revert() - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Revert a rotation/rotation rate pair.

revert() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Revert a rotation/rotation rate pair.

RHUMIDITY - org.orekit.files.ccsds.Keyword

Data: Relative humidity [%].

RinexHeader - Class in org.orekit.gnss

Container for Rinex file header.

RinexHeader(double, SatelliteSystem, String, String, String, String, String, String, String, String, String, String, Vector3D, double, Vector2D, Vector3D, String, Vector3D, Vector3D, double, Vector3D, Vector3D, String, double, AbsoluteDate, AbsoluteDate, int, List<RinexLoader.Parser.AppliedDCBS>, List<RinexLoader.Parser.AppliedPCVS>, List<RinexLoader.Parser.PhaseShiftCorrection>, int, int, int, int) - Constructor for class org.orekit.gnss.RinexHeader

Simple constructor, for Rinex 3 Header.

RinexHeader(double, SatelliteSystem, String, String, String, String, String, String, String, String, String, String, Vector3D, double, Vector2D, Vector3D, Vector3D, Vector3D, double, AbsoluteDate, AbsoluteDate, int, int) - Constructor for class org.orekit.gnss.RinexHeader

Simple constructor, for Rinex 2 Header.

RinexLoader - Class in org.orekit.gnss

Loader for Rinex measurements files.

RinexLoader(InputStream, String) - Constructor for class org.orekit.gnss.RinexLoader

Simple constructor.

RinexLoader(String) - Constructor for class org.orekit.gnss.RinexLoader

Simple constructor.

RinexLoader.Parser - Class in org.orekit.gnss

Parser for rinex files.

RinexLoader.Parser.AppliedDCBS - Class in org.orekit.gnss

Corrections of Differential Code Biases (DCBs) applied.

RinexLoader.Parser.AppliedPCVS - Class in org.orekit.gnss

Corrections of antenna phase center variations (PCVs) applied.

RinexLoader.Parser.PhaseShiftCorrection - Class in org.orekit.gnss

Phase Shift corrections.

RinexLoader.Parser.ScaleFactorCorrection - Class in org.orekit.gnss

Scale Factor to be applied.

rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType

Get the rotation from inertial frame to local orbital frame.

RSW - org.orekit.files.ccsds.CCSDSFrame

Another name for Radial, Transverse (along-track) and Normal.

RTN - org.orekit.files.ccsds.CCSDSFrame

Radial, Transverse (along-track) and Normal.

S

S01 - org.orekit.gnss.Frequency

SBAS L1 (1575.42 MHz).

S05 - org.orekit.gnss.Frequency

SBAS L5 (1176.45 MHz).

S1 - org.orekit.gnss.ObservationType

Doppler GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.

S1A - org.orekit.gnss.ObservationType

Signal-strength Galileo E1 A for Rinex3.

S1B - org.orekit.gnss.ObservationType

Signal-strength Galileo E1 I/NAV OS/CS/SoL for Rinex3.

S1C - org.orekit.gnss.ObservationType

Signal-strength GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.

S1I - org.orekit.gnss.ObservationType

Signal-strength Beidou B1 I for Rinex3.

S1L - org.orekit.gnss.ObservationType

Signal-strength GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3.

S1M - org.orekit.gnss.ObservationType

Signal-strength GPS L2 M for Rinex3.

S1N - org.orekit.gnss.ObservationType

Signal-strength GPS L1 codeless for Rinex3.

S1P - org.orekit.gnss.ObservationType

Signal-strength GPS L2 P(AS off) / GLONASS G2 P for Rinex3.

S1S - org.orekit.gnss.ObservationType

Signal-strength GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3.

S1W - org.orekit.gnss.ObservationType

Signal-strength GPS L1 Z-tracking and similar (AS on) for Rinex3.

S1X - org.orekit.gnss.ObservationType

Signal-strength GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) for Rinex3.

S1Y - org.orekit.gnss.ObservationType

Signal-strength GPS L1 Y for Rinex3.

S1Z - org.orekit.gnss.ObservationType

Signal-strength Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3.

S2 - org.orekit.gnss.ObservationType

Signal Strength GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.

S2 - Static variable in class org.orekit.models.earth.displacement.Tide

S₂ tide.

S2C - org.orekit.gnss.ObservationType

Signal-strength GPS L2 C/A / GLONASS G2 C/A for Rinex3.

S2D - org.orekit.gnss.ObservationType

Signal-strength GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.

S2I - org.orekit.gnss.ObservationType

Signal-strength Beidou B1 I for Rinex3.03.

S2L - org.orekit.gnss.ObservationType

Signal-strength GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.

S2M - org.orekit.gnss.ObservationType

Signal-strength GPS L2 M for Rinex3.

S2N - org.orekit.gnss.ObservationType

Signal-strength GPS L2 codeless for Rinex3.

S2P - org.orekit.gnss.ObservationType

Signal-strength GPS L2 P(AS off) / GLONASS G2 P for Rinex3.

S2Q - org.orekit.gnss.ObservationType

Signal-strength Beidou B1 Q for Rinex3.03.

S2S - org.orekit.gnss.ObservationType

Signal-strength GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.

S2W - org.orekit.gnss.ObservationType

Signal-strength GPS L2 Z-tracking and similar (AS on) for Rinex3.

S2X - org.orekit.gnss.ObservationType

Signal-strength GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3.

S2Y - org.orekit.gnss.ObservationType

Signal-strength GPS L2 Y for Rinex3.

S3I - org.orekit.gnss.ObservationType

Signal-strength GLONASS G3 I for Rinex3.

S3Q - org.orekit.gnss.ObservationType

Signal-strength GLONASS G3 Q for Rinex3.

S3X - org.orekit.gnss.ObservationType

Signal-strength GLONASS G3 I+Q for Rinex3.

s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

s* new value for the contant s.

S5 - org.orekit.gnss.ObservationType

Signal Strength GPS L5 / Galileo E5a / SBAS L5 for Rinex2.

S5A - org.orekit.gnss.ObservationType

Signal-strength IRNSS L5 A for Rinex3.

S5B - org.orekit.gnss.ObservationType

Signal-strength IRNSS L5 B for Rinex3.

S5C - org.orekit.gnss.ObservationType

Signal-strength IRNSS L5 C for Rinex3.

S5I - org.orekit.gnss.ObservationType

Signal-strength GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.

S5Q - org.orekit.gnss.ObservationType

Signal-strength GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.

S5X - org.orekit.gnss.ObservationType

Signal-strength GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C for Rinex3.

S6 - org.orekit.gnss.ObservationType

Signal Strength Galileo E6 / Beidou B03 for Rinex2.

S6A - org.orekit.gnss.ObservationType

Signal-strength Galileo E6 A PRS for Rinex3.

S6B - org.orekit.gnss.ObservationType

Signal-strength Galileo E6 B C/NAV CS for Rinex3.

S6C - org.orekit.gnss.ObservationType

Signal-strength Galileo E6 C no data for Rinex3.

S6I - org.orekit.gnss.ObservationType

Signal-strength Beidou B3 I for Rinex3.

S6L - org.orekit.gnss.ObservationType

Signal-strength QZSS LEX(6) L for Rinex3.

S6Q - org.orekit.gnss.ObservationType

Signal-strength Beidou B3 Q for Rinex3.

S6S - org.orekit.gnss.ObservationType

Signal-strength QZSS LEX(6) S for Rinex3.

S6X - org.orekit.gnss.ObservationType

Signal-strength Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q for Rinex3.

S6Z - org.orekit.gnss.ObservationType

Signal-strength Galileo E6 A+B+C for Rinex3.

S7 - org.orekit.gnss.ObservationType

Signal Strength Galileo E5b / Beidou B02 for Rinex2.

S7I - org.orekit.gnss.ObservationType

Signal-strength Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.

S7Q - org.orekit.gnss.ObservationType

Signal-strength Galileo Q no data / Beidou B2 Q for Rinex3.

S7X - org.orekit.gnss.ObservationType

Signal-strength Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.

S8 - org.orekit.gnss.ObservationType

Signal Strength Galileo E5a+b for Rinex2.

S8I - org.orekit.gnss.ObservationType

Signal-strength Galileo E5(E5a+E5b) I for Rinex3.

S8Q - org.orekit.gnss.ObservationType

Signal-strength Galileo E5(E5a+E5b) Q for Rinex3.

S8X - org.orekit.gnss.ObservationType

Signal-strength Galileo E5(E5a+E5b) I+Q for Rinex3.

S9A - org.orekit.gnss.ObservationType

Signal-strength IRNSS S A for Rinex3.

S9B - org.orekit.gnss.ObservationType

Signal-strength IRNSS S B for Rinex3.

S9C - org.orekit.gnss.ObservationType

Signal-strength IRNSS S C for Rinex3.

S9X - org.orekit.gnss.ObservationType

Signal-strength IRNSS S B+C for Rinex3.

SA - org.orekit.gnss.ObservationType

Signal-strength GPS L1 C/A / GLONASS G1 C/A for Rinex2.

SaastamoinenModel - Class in org.orekit.models.earth

The modified Saastamoinen model.

SaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.SaastamoinenModel

Create a new Saastamoinen model for the troposphere using the given environmental conditions.

sample(SphericalPolygonsSet, double, double) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Sample a zone of interest into a grid sample of geodetic points.

SATELLITE_COLLIDED_WITH_TARGET - org.orekit.errors.OrekitMessages

SatelliteAntenna - Class in org.orekit.gnss.antenna

GNSS satellite antenna model.

SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna

Deprecated.

since 9.3 replaced by SatelliteAntenna(String, String, Map, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate)

SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna

Simple constructor.

SatelliteAntennaCode - Enum in org.orekit.gnss.antenna

Deprecated.

as of 9.3 replaced by SatelliteType

SatelliteSystem - Enum in org.orekit.gnss

Enumerate for satellite system.

SatelliteType - Enum in org.orekit.gnss.antenna

Enumerate for satellite types.

SATURN - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for Saturn.

SATURN - org.orekit.files.ccsds.CenterName

Saturn body.

SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Saturn.

SB - org.orekit.gnss.ObservationType

Signal-strength GPS L1C for Rinex2.

SBAS - org.orekit.gnss.SatelliteSystem

SBAS system.

SC - org.orekit.gnss.ObservationType

Signal-strength GPS L2C for Rinex2.

scale(double, Orbit) - Method in enum org.orekit.orbits.OrbitType

Compute scaling factor for parameters drivers.

scaleChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter scale has been changed.

Scheduler<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation

Interface for generating measurements sequences.

SCLK - org.orekit.files.ccsds.CcsdsTimeScale

Spacecraft Clock.

SD - org.orekit.gnss.ObservationType

Signal-strength GLONASS G2 for Rinex2.

SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SDP4 type of ephemeris.

SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SDP8 type of ephemeris.

SecularAndHarmonic - Class in org.orekit.utils

Class for fitting evolution of osculating orbital parameters.

SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic

Simple constructor.

segment - org.orekit.files.ccsds.Keyword

Segment keyword.

selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.BurstSelector

Select dates within an interval.

selectDates(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.time.DatesSelector

Select dates within an interval.

selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.FixedStepSelector

Select dates within an interval.

selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Selects the extrapolator to use with the selected TLE.

selectionChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter selection status has been changed.

selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType

Get next function transformer in the specified direction.

SEMI_MAJOR_AXIS - org.orekit.files.ccsds.Keyword

Orbit semi-major axis.

SEMParser - Class in org.orekit.gnss

This class reads SEM almanac files and provides GPS almanacs.

SEMParser(String) - Constructor for class org.orekit.gnss.SEMParser

Simple constructor.

SEPTEMBER - org.orekit.time.Month

September.

setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the central body reference radius.

setAngleType(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the angleType.

setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid

Set the angular convergence threshold.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Set the attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.FieldAbstractPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.FieldPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set attitude provider.

setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration

Set the number of slots to use in caches.

setComment(List<String>) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set the maneuvers data comment, each string in the list corresponds to one line of comment.

setComment(List<String>) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Set the meta-data comment.

setCorrectionAngle1(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the correctionAngle1.

setCorrectionAngle2(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the correctionAngle2.

setCorrectionDoppler(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the correctionDoppler.

setCorrectionRange(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the correctionRange.

setCorrectionReceive(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the correctionReceive.

setCorrectionsApplied(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the correctionApplied.

setCorrectionTransmit(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the correctionTransmit.

setCreationDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile

Set the file creation date and time in UTC.

setCurrentWeight(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Deprecated.

as of 9.2, weight should not be changed anymore, rejected measurements are identified by their status

setDataQuality(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the dataQuality.

setDeltaMass(double) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set mass change during maneuver (value is < 0).

setDuration(double) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set duration (value is 0 for impulsive maneuver).

setdV(Vector3D) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set velocity increment.

setElem(int, int, PolynomialFunction) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set an element of the matrix.

setEnabled(boolean) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Enable or disable a measurement.

setEnabled(boolean) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Enable or disable a measurement.

setEOPContinuityThreshold(double) - Static method in class org.orekit.frames.FramesFactory

Set the threshold to check EOP continuity.

setEphemerisMode() - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to ephemeris generation mode.

setEphemerisMode() - Method in class org.orekit.propagation.FieldAbstractPropagator

Set the propagator to ephemeris generation mode.

setEphemerisMode() - Method in interface org.orekit.propagation.FieldPropagator

Set the propagator to ephemeris generation mode.

setEphemerisMode() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the propagator to ephemeris generation mode.

setEphemerisMode() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set the propagator to ephemeris generation mode.

setEphemerisMode() - Method in interface org.orekit.propagation.Propagator

Set the propagator to ephemeris generation mode.

setEphemerisMode(OrekitStepHandler) - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to ephemeris generation mode with the specified handler for each integration step.

setEphemerisMode(OrekitStepHandler) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the propagator to ephemeris generation mode with the specified handler for each integration step.

setEphemerisMode(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator

Set the propagator to ephemeris generation mode with the specified handler for each integration step.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile.Observation

Setter for the epoch.

setEstimatedValue(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Set the estimated value.

setFormatVersion(double) - Method in class org.orekit.files.ccsds.TDMFile

Set the CCSDS ODM (OPM, OMM or OEM) format version.

setFreqOffset(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the freqOffset.

setHeaderComment(List<String>) - Method in class org.orekit.files.ccsds.TDMFile

Set the header comment.

setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Set the initial value of the Jacobian with respect to state and parameter.

setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Set the initial value of the Jacobian with respect to state and parameter.

setInitialJacobians(SpacecraftState, int) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Deprecated.

as of 9.0, replaced by PartialDerivativesEquations.setInitialJacobians(SpacecraftState)

setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set the initial state.

setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set the initial state.

setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the initial state with osculating orbital elements.

setInitialState(SpacecraftState, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the initial state.

setIntegrationInterval(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the integrationInterval.

setIntegrationRef(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the integrationRef.

setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the interpolation grid generator.

setInterpolationGridToMaxTimeGap(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the interpolation grid generator.

setKeyword(String) - Method in class org.orekit.files.ccsds.TDMFile.Observation

Setter for the keyword.

setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Set the given main field coefficients.

setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Set the initial mass.

setMasterMode(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to master mode with fixed steps.

setMasterMode(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator

Set the propagator to master mode with fixed steps.

setMasterMode(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Set the propagator to master mode with variable steps.

setMasterMode(FieldOrekitStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator

Set the propagator to master mode with variable steps.

setMasterMode(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set the propagator to master mode with variable steps.

setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to master mode with variable steps.

setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the propagator to master mode with variable steps.

setMasterMode(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator

Set the propagator to master mode with variable steps.

setMasterMode(T, FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Set the propagator to master mode with fixed steps.

setMasterMode(T, FieldOrekitFixedStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator

Set the propagator to master mode with fixed steps.

setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set values for all elements.

setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set the value of a line of the matrix.

setMaxEvaluations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set the maximum number of model evaluations.

setMaxIterations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set the maximum number of iterations.

setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Set the degree limit for the next file parsing.

setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the degree limit for the next file parsing.

setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Set the order limit for the next file parsing.

setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the order limit for the next file parsing.

setMaxValue(double) - Method in class org.orekit.utils.ParameterDriver

Set maximum parameter value.

setMeasurement(double) - Method in class org.orekit.files.ccsds.TDMFile.Observation

Setter for the measurement.

setMetaData(TDMFile.TDMMetaData) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Set the meta-data for the block.

setMinValue(double) - Method in class org.orekit.utils.ParameterDriver

Set minimum parameter value.

setMode(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the mode.

setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the central body attraction coefficient.

setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the central attraction coefficient μ.

setMu(double) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set the central attraction coefficient μ.

setMu(double) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set the central attraction coefficient μ.

setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set the central attraction coefficient μ.

setMuUsed() - Method in class org.orekit.files.ccsds.ODMFile

Set the gravitational coefficient created from the knowledge of the central body.

setName(String) - Method in class org.orekit.utils.ParameterDriver

Change the name of this parameter driver.

setNormalizedValue(double) - Method in class org.orekit.utils.ParameterDriver

Set normalized value.

setObservations(List<TDMFile.Observation>) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Set the list of Observations Data Lines.

setObservationsBlocks(List<TDMFile.ObservationsBlock>) - Method in class org.orekit.files.ccsds.TDMFile

Set the list of Observations Blocks.

setObservationsComment(List<String>) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock

Set the observations data lines comment.

setObserver(BatchLSObserver) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set an observer for iterations.

setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.KalmanEstimator

Set the observer.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set propagation orbit type.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set propagation orbit type.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set propagation orbit type.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set propagation orbit type.

setOriginator(String) - Method in class org.orekit.files.ccsds.TDMFile

Set the file originator.

setParameterDerivatives(ParameterDriver, double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Set the partial derivatives of the simulated measurement with respect to parameter.

setParameters(double[]) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Set the selected parameters.

setParametersConvergenceThreshold(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set convergence threshold.

setParticipants(Map<Integer, String>) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the participants.

setPath(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the path.

setPath1(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the path1.

setPath2(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the path2.

setPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper

Set position angle type.

setPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper

Set position angle type.

setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set position angle type.

setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set position angle type.

setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set position angle type.

setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set position angle type.

setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Set the local pressure at the evaluation location

setRangeMode(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the rangeMode.

setRangeModulus(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the rangeModulus.

setRangeUnits(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the rangeUnits.

setRawCoefficients(boolean, double[][], double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the tesseral-sectorial coefficients matrix.

setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the indicator for completed read.

setReceiveBand(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the receiveBand.

setReceiveDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the receiveDelays.

setReferenceDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Set reference date.

setReferenceFrame(Frame) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Set the reference frame in which data are given: used for RADEC tracking data.

setReferenceFrameString(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Set the reference frame name.

setReferenceValue(double) - Method in class org.orekit.utils.ParameterDriver

Set reference parameter value.

setRefFrame(Frame) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set Coordinate system for velocity increment vector, for absolute frames.

setRefLofType(LOFType) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set coordinate system for velocity increment vector, for Local Orbital Frames.

setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Allow/disallow resetting the initial state at end of propagation.

setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Allow/disallow resetting the initial state at end of propagation.

setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Override the default value of the parameter.

setScale(double) - Method in class org.orekit.utils.ParameterDriver

Set scale.

setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Set the given secular variation coefficients.

setSelected(boolean) - Method in class org.orekit.utils.ParameterDriver

Configure a parameter selection status.

setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the selected short periodic coefficients that must be stored as additional states.

setSigma(double[]) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter

Set the current value of sigma.

setSlaveMode() - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to slave mode.

setSlaveMode() - Method in class org.orekit.propagation.FieldAbstractPropagator

Set the propagator to slave mode.

setSlaveMode() - Method in interface org.orekit.propagation.FieldPropagator

Set the propagator to slave mode.

setSlaveMode() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the propagator to slave mode.

setSlaveMode() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set the propagator to slave mode.

setSlaveMode() - Method in interface org.orekit.propagation.Propagator

Set the propagator to slave mode.

setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator

Set a start date.

setStartDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Set a start date.

setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the startTime.

setStartTimeString(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the startTime String.

setStateDerivatives(int, double[]...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Set the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.

setStatus(EstimatedMeasurement.Status) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Set the status.

setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the stopTime.

setStopTimeString(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the stopTime String.

setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Set the local temperature at the evaluation location

setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the TideSystem used in the gravity field.

setTimeout(int) - Method in class org.orekit.data.NetworkCrawler

Set the timeout for connection.

setTimeSystem(CcsdsTimeScale) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Set the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.

setTimetagRef(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the timetagRef.

setTransmitBand(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the transmitBand.

setTransmitDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the transmitDelays.

setTurnaroundDenominator(int) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the turnaroundDenominator.

setTurnaroundNumerator(int) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData

Setter for the turnaroundNumerator.

setUpEventDetector(FieldODEIntegrator<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Wrap an Orekit event detector and register it to the integrator.

setUpEventDetector(ODEIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Wrap an Orekit event detector and register it to the integrator.

setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set up all user defined event detectors.

setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set up all user defined event detectors.

setValue(double) - Method in class org.orekit.utils.ParameterDriver

Set parameter value.

SEVERAL_REFERENCE_DATES_IN_GRAVITY_FIELD - org.orekit.errors.OrekitMessages

SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP type of ephemeris.

SGP4 - Class in org.orekit.propagation.analytical.tle

This class contains methods to compute propagated coordinates with the SGP4 model.

SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP4 type of ephemeris.

SGP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.SGP4

Constructor for a unique initial TLE.

SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP8 type of ephemeris.

shiftedBy(double) - Method in class org.orekit.attitudes.Attitude

Get a time-shifted attitude.

shiftedBy(double) - Method in class org.orekit.attitudes.FieldAttitude

Get a time-shifted attitude.

shiftedBy(double) - Method in class org.orekit.frames.FieldTransform

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.frames.Transform

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.FieldCartesianOrbit

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.orbits.FieldCircularOrbit

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.Orbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.propagation.FieldSpacecraftState

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate

Get a time-shifted date.

shiftedBy(double) - Method in class org.orekit.time.FieldAbsoluteDate

Get a time-shifted date.

shiftedBy(double) - Method in interface org.orekit.time.FieldTimeShiftable

Get a time-shifted instance.

shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates

Get a time-shifted state.

shiftedBy(KK) - Method in interface org.orekit.time.FieldTimeShiftable

Get a time-shifted instance.

shiftedBy(T) - Method in class org.orekit.attitudes.FieldAttitude

Get a time-shifted attitude.

shiftedBy(T) - Method in class org.orekit.frames.FieldTransform

Get a time-shifted instance.

shiftedBy(T) - Method in class org.orekit.orbits.FieldCartesianOrbit

Get a time-shifted orbit.

shiftedBy(T) - Method in class org.orekit.orbits.FieldCircularOrbit

Get a time-shifted orbit.

shiftedBy(T) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get a time-shifted orbit.

shiftedBy(T) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get a time-shifted orbit.

shiftedBy(T) - Method in class org.orekit.orbits.FieldOrbit

Get a time-shifted orbit.

shiftedBy(T) - Method in class org.orekit.propagation.FieldSpacecraftState

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.time.FieldAbsoluteDate

Get a time-shifted date.

shiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Get a time-shifted state.

ShiftingTransformProvider - Class in org.orekit.frames

Transform provider using thread-safe shifts on transforms sample.

ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider

Simple constructor.

ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider

Deprecated.

as of 9.1, replaced by ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double)

SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for SHM files.

SHMFormatReader - Class in org.orekit.forces.gravity.potential

Reader for the SHM gravity field format.

SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader

Simple constructor.

ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolated short periodics coefficients.

ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Simple constructor.

ShortPeriodTerms - Interface in org.orekit.propagation.semianalytical.dsst.forces

Additive short period terms contributing to the mean to osculating orbit mapping.

SIGNAL_STRENGTH - org.orekit.gnss.MeasurementType

Signal-strength measurement.

signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement

Compute propagation delay on a link leg (typically downlink or uplink).

signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement

Compute propagation delay on a link leg (typically downlink or uplink).

signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.AbstractParametricAcceleration

Compute the signed amplitude of the acceleration.

signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.HarmonicParametricAcceleration

Compute the signed amplitude of the acceleration.

signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.PolynomialParametricAcceleration

Compute the signed amplitude of the acceleration.

signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.AbstractParametricAcceleration

Compute the signed amplitude of the acceleration.

signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.HarmonicParametricAcceleration

Compute the signed amplitude of the acceleration.

signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.PolynomialParametricAcceleration

Compute the signed amplitude of the acceleration.

SignSemantic - Enum in org.orekit.estimation.measurements.generation

Enumerate for the semantic of the g function sign during measurements generation.

SimpleExponentialAtmosphere - Class in org.orekit.forces.drag.atmosphere

Simple exponential atmospheric model.

SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere

Create an exponential atmosphere.

SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data

Parser for simple tables containing time stamped data.

SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser

Simple constructor.

SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data

Interface for converting a table row into time-stamped data.

SINGULAR_JACOBIAN_FOR_ORBIT_TYPE - org.orekit.errors.OrekitMessages

sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

sinus original inclination.

SLAVE_MODE - Static variable in interface org.orekit.propagation.FieldPropagator

Indicator for slave mode.

SLAVE_MODE - Static variable in interface org.orekit.propagation.Propagator

Indicator for slave mode.

SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers

Analytical model for small maneuvers.

SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Build a maneuver defined in spacecraft frame.

SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Build a maneuver defined in user-specified frame.

SOLAR_RAD_AREA - org.orekit.files.ccsds.Keyword

Solar radiation pressure area.

SOLAR_RAD_COEFF - org.orekit.files.ccsds.Keyword

Solar radiation pressure coefficient.

SOLAR_SYSTEM_BARYCENTER - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for solar system barycenter.

SOLAR_SYSTEM_BARYCENTER - org.orekit.files.ccsds.CenterName

Solar system barycenter aggregated body.

SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for solar system barycenter.

SolarRadiationPressure - Class in org.orekit.forces.radiation

Solar radiation pressure force model.

SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure

Complete constructor.

SolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure

Deprecated.

as of 9.2 replaced by SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive)

SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure

Simple constructor with default reference values.

SolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure

Deprecated.

as of 9.2 replaced by SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive)

SolidTides - Class in org.orekit.forces.gravity

Solid tides force model.

SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides

Simple constructor.

SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides

Simple constructor.

sort() - Method in class org.orekit.utils.ParameterDriversList

Sort the parameters lexicographically.

SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3File

String representation of the center of ephemeris coordinate system.

SP3_NUMBER_OF_EPOCH_MISMATCH - org.orekit.errors.OrekitMessages

SP3_UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages

SP3_UNSUPPORTED_VERSION - org.orekit.errors.OrekitMessages

SP3File - Class in org.orekit.files.sp3

Represents a parsed SP3 orbit file.

SP3File.SP3Coordinate - Class in org.orekit.files.sp3

A single record of position clock and possibly derivatives in an SP3 file.

SP3File.SP3Ephemeris - Class in org.orekit.files.sp3

An ephemeris for a single satellite in a SP3 file.

SP3File.SP3FileType - Enum in org.orekit.files.sp3

File type indicator.

SP3File.SP3OrbitType - Enum in org.orekit.files.sp3

Orbit type indicator.

SP3File.TimeSystem - Enum in org.orekit.files.sp3

Time system used throughout this SP3 file.

SP3Parser - Class in org.orekit.files.sp3

A parser for the SP3 orbit file format.

SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser

Create an SP3 parser using default values.

SP3Parser(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3Parser

Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.

SPACECRAFT_MASS_BECOMES_NEGATIVE - org.orekit.errors.OrekitMessages

SpacecraftState - Class in org.orekit.propagation

This class is the representation of a complete state holding orbit, attitude and mass information at a given date.

SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit only.

SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState

Create a new instance from orbit and mass.

SpacecraftState(Orbit, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState

Create a new instance from orbit and mass.

SpacecraftState(Orbit, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit only.

SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit and attitude provider.

SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit, attitude provider and mass.

SpacecraftState(Orbit, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit, attitude provider and mass.

SpacecraftState(Orbit, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit and attitude provider.

SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants

Speed of light: 299792458.0 m/s.

SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide spherical harmonics coefficients.

SphericalPolygonsSetTransferObject - Class in org.orekit.utils

Transfer object for serializing SphericalPolygonsSet instances.

SphericalPolygonsSetTransferObject(SphericalPolygonsSet) - Constructor for class org.orekit.utils.SphericalPolygonsSetTransferObject

Simple constructor.

SpinStabilized - Class in org.orekit.attitudes

This class handles a spin stabilized attitude provider.

SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized

Creates a new instance.

SSA - Static variable in class org.orekit.models.earth.displacement.Tide

Ssa tide.

STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

NIST standard atmospheric pressure (Pa).

STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

NIST standard atmospheric temperature (K).

START_TIME - org.orekit.files.ccsds.Keyword

Start of total time span covered by:

startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Start parsing.

STATE_AND_PARAMETERS_JACOBIANS_ROWS_MISMATCH - org.orekit.errors.OrekitMessages

STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.JacobiansMapper

State dimension, fixed to 6.

STATE_JACOBIAN_NOT_6X6 - org.orekit.errors.OrekitMessages

STATE_JACOBIAN_NOT_INITIALIZED - org.orekit.errors.OrekitMessages

StateFunction - Interface in org.orekit.utils

Interface representing a vector function depending on SpacecraftState.

StateJacobian - Interface in org.orekit.utils

Interface representing the Jacobian of a vector function depending on SpacecraftState.

StateMapper - Class in org.orekit.propagation.integration

This class maps between raw double elements and SpacecraftState instances.

StateMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper

Simple constructor.

STATION_NOT_FOUND - org.orekit.errors.OrekitMessages

StationDisplacement - Interface in org.orekit.models.earth.displacement

Interface for computing reference points displacement.

STEC - org.orekit.files.ccsds.Keyword

Data: STEC - Slant Total Electron Count [TECU].

stillAcceptsData() - Method in interface org.orekit.data.DataLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.gnss.RinexLoader.Parser

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.gnss.SEMParser

stillAcceptsData() - Method in class org.orekit.gnss.YUMAParser

stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader

stillAcceptsData() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader

Check if the loader still accepts new data.

STOP - org.orekit.propagation.events.handlers.EventHandler.Action

Stop indicator.

STOP - org.orekit.propagation.events.handlers.FieldEventHandler.Action

Stop indicator.

STOP_TIME - org.orekit.files.ccsds.Keyword

End of total time span covered by:

StopOnDecreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing

StopOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Event handler which will always return stop as a state.

StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent

StopOnIncreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing

StreamingOemWriter - Class in org.orekit.files.ccsds

A writer for OEM files.

StreamingOemWriter(Appendable, TimeScale, Map<Keyword, String>) - Constructor for class org.orekit.files.ccsds.StreamingOemWriter

Create an OEM writer than streams data to the given output stream.

StreamingOemWriter.Segment - Class in org.orekit.files.ccsds

A writer for a segment of an OEM.

STRONG - org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel

Strong level of activity.

subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Subtract an offset from the instance.

subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Subtract an offset from the instance.

subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Subtract an offset from the instance.

subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Subtract an offset from the instance.

SUN - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for the Sun.

SUN - org.orekit.files.ccsds.CenterName

Sun body.

SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Sun.

SUN_RADIUS - Static variable in interface org.orekit.utils.Constants

Sun radius: 695500000 m.

supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField

Indicates whether this model supports time transformation or not.

switchOccurred(AttitudeProvider, AttitudeProvider, SpacecraftState) - Method in interface org.orekit.attitudes.AttitudesSequence.SwitchHandler

Method called when attitude is switched from one law to another law.

sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.SGP4

Initialization proper to each propagator (SGP or SDP).

sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Initialization proper to each propagator (SGP or SDP).

sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.SGP4

Propagation proper to each propagator (SGP or SDP).

sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Propagation proper to each propagator (SGP or SDP).

T

t2cof - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

3/2 * C1.

TabulatedLofOffset - Class in org.orekit.attitudes

This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.

TabulatedLofOffset(Frame, LOFType, List<TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedLofOffset

Creates new instance.

TabulatedProvider - Class in org.orekit.attitudes

This class handles an attitude provider interpolating from a predefined table.

TabulatedProvider(Frame, List<TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedProvider

Creates new instance.

TAI - org.orekit.files.ccsds.CcsdsTimeScale

International Atomic Time.

TAI - org.orekit.files.sp3.SP3File.TimeSystem

International Atomic Time.

TAIScale - Class in org.orekit.time

International Atomic Time.

TAIUTCDatFilesLoader - Class in org.orekit.time

Loader for UTC-TAI extracted from tai-utc.dat file from USNO.

TAIUTCDatFilesLoader(String) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader

Build a loader for tai-utc.dat file from USNO.

TargetPointing - Class in org.orekit.attitudes

This class handles target pointing attitude provider.

TargetPointing(Frame, GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing

Creates a new instance from body shape and target expressed in geodetic coordinates.

TargetPointing(Frame, Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing

Creates a new instance from body frame and target expressed in Cartesian coordinates.

TCB - org.orekit.files.ccsds.CcsdsTimeScale

Barycentric Coordinate Time.

TCBScale - Class in org.orekit.time

Barycentric Coordinate Time.

TCG - org.orekit.files.ccsds.CcsdsTimeScale

Geocentric Coordinate Time.

TCGScale - Class in org.orekit.time

Geocentric Coordinate Time.

TDB - org.orekit.files.ccsds.CcsdsTimeScale

Barycentric Dynamical Time.

TDBScale - Class in org.orekit.time

Barycentric Dynamic Time.

tdm - org.orekit.files.ccsds.Keyword

TDM first keyword.

TDMFile - Class in org.orekit.files.ccsds

This class stocks all the information of the CCSDS Tracking Data Message file parsed by TDMParser or TDMXMLParser.

TDMFile() - Constructor for class org.orekit.files.ccsds.TDMFile

OEMFile constructor.

TDMFile.Observation - Class in org.orekit.files.ccsds

The Observation class contains the data from an observation line.

TDMFile.ObservationsBlock - Class in org.orekit.files.ccsds

The Observations Block class contain metadata and the list of observation data lines.

TDMFile.TDMMetaData - Class in org.orekit.files.ccsds

The TDMMetadata class gathers the meta-data present in the Tracking Data Message (TDM).

TDMMetaData() - Constructor for class org.orekit.files.ccsds.TDMFile.TDMMetaData

Create a new TDM meta-data.

TDMParser - Class in org.orekit.files.ccsds

Class for CCSDS Tracking Data Message parsers.

TDMParser() - Constructor for class org.orekit.files.ccsds.TDMParser

Simple constructor.

TDMParser.TDMFileFormat - Enum in org.orekit.files.ccsds

Enumerate for the format.

TDR - org.orekit.files.ccsds.CCSDSFrame

True of Date, Rotating.

TEME - org.orekit.files.ccsds.CCSDSFrame

True Equator Mean Equinox.

TEME - org.orekit.frames.Predefined

TEME frame.

TEMPERATURE - org.orekit.files.ccsds.Keyword

Data: Temperature [K].

tessellate(SphericalPolygonsSet, double, double, double, double, boolean, boolean) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Tessellate a zone of interest into tiles.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularAzEl

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularRaDec

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.InterSatellitesRange

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Phase

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Position

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.PV

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Range

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.RangeRate

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TurnAroundRange

Estimate the theoretical value.

theta2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

cos io squared.

ThirdBodyAttraction - Class in org.orekit.forces.gravity

Third body attraction force model.

ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction

Simple constructor.

ThreeEighthesIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for ThreeEighthesIntegrator.

ThreeEighthesIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder

Build a new instance.

THRUST - Static variable in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Parameter name for thrust.

TidalDisplacement - Class in org.orekit.models.earth.displacement

Modeling of displacement of reference points due to tidal effects.

TidalDisplacement(double, double, double, PVCoordinatesProvider, PVCoordinatesProvider, IERSConventions, boolean) - Constructor for class org.orekit.models.earth.displacement.TidalDisplacement

Simple constructor.

Tide - Class in org.orekit.models.earth.displacement

Class representing a tide.

Tide(int) - Constructor for class org.orekit.models.earth.displacement.Tide

Simple constructor.

Tide(int, int, int, int, int, int) - Constructor for class org.orekit.models.earth.displacement.Tide

Simple constructor.

TIDE_FREE - org.orekit.forces.gravity.potential.TideSystem

Constant for tide-free gravity fields.

TideSystem - Enum in org.orekit.forces.gravity.potential

Enumerate for tie systems.

TideSystemProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide tide systems.

Tile - Class in org.orekit.models.earth.tessellation

Simple data structure for a quadrilateral tile shape on a body surface.

Tile(GeodeticPoint, GeodeticPoint, GeodeticPoint, GeodeticPoint) - Constructor for class org.orekit.models.earth.tessellation.Tile

Create a tile.

TileAiming - Interface in org.orekit.models.earth.tessellation

Interface defining the aiming direction of tiles.

TIME_SYSTEM - org.orekit.files.ccsds.Keyword

Time system used for state vector, maneuver, and covariance data.

TimeComponents - Class in org.orekit.time

Class representing a time within the day broken up as hour, minute and second components.

TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents

Build a time from the second number within the day.

TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents

Build a time from the second number within the day.

TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents

Build a time from its clock elements.

TimeComponents(int, int, double, int) - Constructor for class org.orekit.time.TimeComponents

Build a time from its clock elements.

TimeDerivativesEquations - Interface in org.orekit.propagation.numerical

Interface summing up the contribution of several forces into orbit and mass derivatives.

TimeInterpolable<T extends TimeInterpolable<T>> - Interface in org.orekit.time

This interface represents objects that can be interpolated in time.

TimeScalarFunction - Interface in org.orekit.time

This interface represents a scalar function of time.

TimeScale - Interface in org.orekit.time

Interface for time scales.

TimeScalesFactory - Class in org.orekit.time

Factory for predefined time scales.

timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Compute the offset between two time scales at the current instant.

timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Compute the offset between two time scales at the current instant.

TimeShiftable<T extends TimeShiftable<T>> - Interface in org.orekit.time

This interface represents objects that can be shifted in time.

TimeSpanMap<T> - Class in org.orekit.utils

Container for objects that apply to spans of time.

TimeSpanMap(T) - Constructor for class org.orekit.utils.TimeSpanMap

Create a map containing a single object, initially valid throughout the timeline.

TimeSpanMap.Span<S> - Class in org.orekit.utils

Holder for one time span.

TimeSpanMap.Transition<S> - Class in org.orekit.utils

Class holding transition times.

TimeStamped - Interface in org.orekit.time

This interface represents objects that have a AbsoluteDate date attached to them.

TimeStampedAngularCoordinates - Class in org.orekit.utils

time-stamped version of AngularCoordinates.

TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Builds a TimeStampedAngularCoordinates from a FieldRotation<DerivativeStructure>.

TimeStampedAngularCoordinates(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Builds a rotation/rotation rate pair.

TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Build one of the rotations that transform one pv coordinates into another one.

TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another pair.

TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils

Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.

TimeStampedCacheException - Exception in org.orekit.errors

This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.

TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(MathRuntimeException) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedFieldAngularCoordinates<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.utils

time-stamped version of FieldAngularCoordinates.

TimeStampedFieldAngularCoordinates(Field<T>, TimeStampedAngularCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds an instance for a regular TimeStampedAngularCoordinates.

TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds a rotation/rotation rate pair.

TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another pair.

TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds a TimeStampedFieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.

TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds a rotation/rotation rate pair.

TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another pair.

TimeStampedFieldPVCoordinates<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.utils

time-stamped version of FieldPVCoordinates.

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Builds a PVCoordinates pair.

TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Basic constructor.

TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Subtractive constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Builds a TimeStampedFieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Builds a PVCoordinates pair.

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Basic constructor.

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Subtractive constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedGenerator<T extends TimeStamped> - Interface in org.orekit.utils

Generator to use for creating entries in time stamped caches.

TimeStampedPVCoordinates - Class in org.orekit.utils

time-stamped version of PVCoordinates.

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Multiplicative constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Builds a TimeStampedPVCoordinates triplet from a FieldVector3D<DerivativeStructure>.

TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Build from position and velocity.

TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Builds a TimeStampedPVCoordinates pair.

TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Build from position velocity acceleration coordinates.

TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Subtractive constructor

TIMETAG_REF - org.orekit.files.ccsds.Keyword

Meta-data: Timetag reference.

TimeVectorFunction - Interface in org.orekit.time

This interface represents a multi-valued function of time.

TIRF_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined

TIRF, IERS 996 conventions, with accurate EOP interpolation.

TIRF_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined

TIRF, IERS 1996 conventions, with simple EOP interpolation.

TIRF_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined

TIRF, IERS 2003 conventions, with accurate EOP interpolation.

TIRF_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined

TIRF, IERS 2003 conventions, with simple EOP interpolation.

TIRF_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined

TIRF, IERS 2010 conventions, with accurate EOP interpolation.

TIRF_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined

TIRF, IERS 2010 conventions, with simple EOP interpolation.

tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

Initial state.

TLE - Class in org.orekit.propagation.analytical.tle

This class is a container for a single set of TLE data.

TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.TLE

Simple constructor from already parsed elements.

TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE

Simple constructor from unparsed two lines.

TLE_CHECKSUM_ERROR - org.orekit.errors.OrekitMessages

TLE_INVALID_PARAMETER - org.orekit.errors.OrekitMessages

TLE_LINES_DO_NOT_REFER_TO_SAME_OBJECT - org.orekit.errors.OrekitMessages

TLEPropagator - Class in org.orekit.propagation.analytical.tle

This class provides elements to propagate TLE's.

TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator

Protected constructor for derived classes.

TLEPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for TLEPropagator.

TLEPropagatorBuilder(TLE, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder

Build a new instance.

TLESeries - Class in org.orekit.propagation.analytical.tle

Deprecated.

as of 9.0, this class is deprecated without replacement. The file format used was considered to be too specific and the API not really well designed. Users are encouraged to use their own parser for series of TLE

TLESeries(String, boolean) - Constructor for class org.orekit.propagation.analytical.tle.TLESeries

Deprecated.

Simple constructor with a TLE file.

TNW - org.orekit.files.ccsds.CCSDSFrame

TNW : x-axis along the velocity vector, W along the orbital angular momentum vector and N completes the right handed system.

TNW - org.orekit.frames.LOFType

Constant for TNW frame (X axis aligned with velocity, Z axis aligned with orbital momentum).

toAbsoluteDate() - Method in class org.orekit.time.FieldAbsoluteDate

Transform the FieldAbsoluteDate in an AbsoluteDate.

toAngularCoordinates() - Method in class org.orekit.utils.FieldAngularCoordinates

Convert to a regular angular coordinates.

toArray(List<List<Double>>) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Convert a list of list into an array.

toAttitude() - Method in class org.orekit.attitudes.FieldAttitude

Converts to an Attitude instance.

TOD - org.orekit.files.ccsds.CCSDSFrame

True of Date.

TOD_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined

TOD, IERS 1996 conventions, with accurate EOP interpolation.

TOD_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined

TOD, IERS 1996 conventions, with simple EOP interpolation.

TOD_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined

TOD, IERS 2003 conventions, with accurate EOP interpolation.

TOD_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined

TOD, IERS 2003 conventions, with simple EOP interpolation.

TOD_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined

TOD, IERS 2010 conventions, with accurate EOP interpolation.

TOD_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined

TOD, IERS 2010 conventions, with simple EOP interpolation.

TOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined

TOD, IERS 1996 conventions without EOP corrections.

toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Convert the instance to a Java Date.

toDate(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Convert the instance to a Java Date.

toDerivativeStructurePV(int) - Method in class org.orekit.utils.FieldPVCoordinates

Transform the instance to a FieldPVCoordinates<FieldDerivativeStructure>.

toDerivativeStructurePV(int) - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldPVCoordinates<DerivativeStructure>.

toDerivativeStructureRotation(int) - Method in class org.orekit.utils.AngularCoordinates

Transform the instance to a FieldRotation<DerivativeStructure>.

toDerivativeStructureRotation(int) - Method in class org.orekit.utils.FieldAngularCoordinates

Transform the instance to a FieldRotation<FieldDerivativeStructure>.

toDerivativeStructureVector(int) - Method in class org.orekit.utils.FieldPVCoordinates

Transform the instance to a FieldVector3D<FieldDerivativeStructure>.

toDerivativeStructureVector(int) - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldVector3D<DerivativeStructure>.

toEquinox(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter

Convert nutation corrections.

toFieldPVCoordinatesProvider(Field<T>) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider

Convert to a FieldPVCoordinatesProvider with a specific type.

toGeodetic(S2Point) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Convert a point on the unit 2-sphere to geodetic coordinates.

tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.

tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator

Estimate tolerance vectors for integrators.

tolerances(T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Estimate tolerance vectors for integrators.

ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

2 / (n² * a) .

toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter

Convert nutation corrections.

TOO_LARGE_DEGREE_FOR_GRAVITY_FIELD - org.orekit.errors.OrekitMessages

TOO_LARGE_ECCENTRICITY_FOR_PROPAGATION_MODEL - org.orekit.errors.OrekitMessages

TOO_LARGE_ORDER_FOR_GRAVITY_FIELD - org.orekit.errors.OrekitMessages

TOO_SHORT_TRANSITION_TIME_FOR_ATTITUDES_SWITCH - org.orekit.errors.OrekitMessages

TOO_SMALL_SCALE_FOR_PARAMETER - org.orekit.errors.OrekitMessages

toOrbit() - Method in class org.orekit.orbits.FieldCartesianOrbit

toOrbit() - Method in class org.orekit.orbits.FieldCircularOrbit

toOrbit() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

toOrbit() - Method in class org.orekit.orbits.FieldKeplerianOrbit

toOrbit() - Method in class org.orekit.orbits.FieldOrbit

Transforms the FieldOrbit instance into an Orbit instance.

toPlane(Vector3D) - Method in class org.orekit.bodies.Ellipse

Project a point to the ellipse plane.

TopocentricFrame - Class in org.orekit.frames

Topocentric frame.

TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame

Simple constructor.

toPVCoordinates() - Method in class org.orekit.utils.FieldPVCoordinates

Convert to a constant position-velocity.

toSI(double) - Method in enum org.orekit.data.PolynomialParser.Unit

Convert value from instance unit to corresponding SI unit.

toSpace(Vector2D) - Method in class org.orekit.bodies.Ellipse

Create a point from its ellipse-relative coordinates.

toSpacecraftState() - Method in class org.orekit.propagation.FieldSpacecraftState

To convert a FieldSpacecraftState instance into a SpacecraftState instance.

toString() - Method in class org.orekit.bodies.FieldGeodeticPoint

toString() - Method in class org.orekit.bodies.GeodeticPoint

toString() - Method in class org.orekit.frames.Frame

New definition of the java.util toString() method.

toString() - Method in class org.orekit.frames.OrphanFrame

toString() - Method in class org.orekit.models.earth.GeoMagneticElements

toString() - Method in class org.orekit.orbits.CartesianOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.CircularOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.EquinoctialOrbit

Returns a string representation of this equinoctial parameters object.

toString() - Method in class org.orekit.orbits.FieldCartesianOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.FieldCircularOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Returns a string representation of this equinoctial parameters object.

toString() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Returns a string representation of this Keplerian parameters object.

toString() - Method in class org.orekit.orbits.KeplerianOrbit

Returns a string representation of this Keplerian parameters object.

toString() - Method in class org.orekit.propagation.analytical.tle.TLE

Get a string representation of this TLE set.

toString() - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location in UTC time scale.

toString() - Method in class org.orekit.time.BDTScale

toString() - Method in class org.orekit.time.DateComponents

Get a string representation (ISO-8601) of the date.

toString() - Method in class org.orekit.time.DateTimeComponents

Return a string representation of this pair.

toString() - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location in UTC time scale.

toString() - Method in class org.orekit.time.GalileoScale

toString() - Method in class org.orekit.time.GLONASSScale

toString() - Method in class org.orekit.time.GMSTScale

toString() - Method in class org.orekit.time.GPSScale

toString() - Method in class org.orekit.time.IRNSSScale

toString() - Method in class org.orekit.time.QZSSScale

toString() - Method in class org.orekit.time.TAIScale

toString() - Method in class org.orekit.time.TCBScale

toString() - Method in class org.orekit.time.TCGScale

toString() - Method in class org.orekit.time.TDBScale

toString() - Method in class org.orekit.time.TimeComponents

Get a string representation of the time.

toString() - Method in class org.orekit.time.TTScale

toString() - Method in class org.orekit.time.UT1Scale

toString() - Method in class org.orekit.time.UTCScale

toString() - Method in class org.orekit.utils.FieldPVCoordinates

Return a string representation of this position/velocity pair.

toString() - Method in class org.orekit.utils.ImmutableTimeStampedCache

toString() - Method in class org.orekit.utils.ParameterDriver

Get a text representation of the parameter.

toString() - Method in class org.orekit.utils.PVCoordinates

Return a string representation of this position/velocity pair.

toString() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Return a string representation of this position/velocity pair.

toString() - Method in class org.orekit.utils.TimeStampedPVCoordinates

Return a string representation of this position/velocity pair.

toString(int) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location for a local time.

toString(int) - Method in class org.orekit.time.DateTimeComponents

Return a string representation of this pair.

toString(int) - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location for a local time.

toString(TimeZone) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location for a time zone.

toString(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location for a time zone.

toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location.

toString(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location.

TOTAL_ZENITH_DELAY - Static variable in class org.orekit.models.earth.EstimatedTroposphericModel

Name of the parameter of this model: the total zenith delay.

toTaylorProvider(Frame) - Method in class org.orekit.utils.TimeStampedPVCoordinates

Create a local provider using simply Taylor expansion through TimeStampedPVCoordinates.shiftedBy(double).

toTimeStampedPVCoordinates() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Convert to a constant position-velocity.

toTransform() - Method in class org.orekit.propagation.FieldSpacecraftState

Compute the transform from orbite/attitude reference frame to spacecraft frame.

toTransform() - Method in class org.orekit.propagation.SpacecraftState

Compute the transform from orbite/attitude reference frame to spacecraft frame.

TRAJECTORY_INSIDE_BRILLOUIN_SPHERE - org.orekit.errors.OrekitMessages

transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape

Transform a Cartesian point to a surface-relative point.

transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a Cartesian point to a surface-relative point.

transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid

Transform a Cartesian point to a surface-relative point.

transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape

Transform a Cartesian point to a surface-relative point.

transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a Cartesian point to a surface-relative point.

transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid

Transform a Cartesian point to a surface-relative point.

transform(FieldGeodeticPoint<T>) - Method in interface org.orekit.bodies.BodyShape

Transform a surface-relative point to a Cartesian point.

transform(FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a surface-relative point to a Cartesian point.

transform(FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.Geoid

Transform a surface-relative point to a Cartesian point.

transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape

Transform a surface-relative point to a Cartesian point.

transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a surface-relative point to a Cartesian point.

transform(GeodeticPoint) - Method in class org.orekit.models.earth.Geoid

Transform a surface-relative point to a Cartesian point.

transform(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a Cartesian point to a surface-relative point.

Transform - Class in org.orekit.frames

Transformation class in three dimensional space.

Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform.

Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first time derivative.

Transform(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first and second time derivatives.

Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform

Build a transform by combining two existing ones.

Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first time derivative.

transformFromInertial(AbsoluteDate, PVCoordinates) - Method in enum org.orekit.frames.LOFType

Get the transform from an inertial frame defining position-velocity and the local orbital frame.

transformFromInertial(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType

Get the transform from an inertial frame defining position-velocity and the local orbital frame.

TransformGenerator - Class in org.orekit.frames

Generator to use transforms in GenericTimeStampedCache.

TransformGenerator(int, TransformProvider, double) - Constructor for class org.orekit.frames.TransformGenerator

simple constructor.

transformLine(FieldLine<T>) - Method in class org.orekit.frames.FieldTransform

Transform a line.

transformLine(Line) - Method in class org.orekit.frames.FieldTransform

Transform a line.

transformLine(Line) - Method in class org.orekit.frames.Transform

Transform a line.

transformModel(double) - Method in class org.orekit.models.earth.GeoMagneticField

Time transform the model coefficients from the base year of the model using secular variation coefficients.

transformModel(GeoMagneticField, double) - Method in class org.orekit.models.earth.GeoMagneticField

Time transform the model coefficients from the base year of the model using a linear interpolation with a second model.

transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.FieldTransform

Transform a position vector (including translation effects).

transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.Transform

Transform a position vector (including translation effects).

transformPosition(Vector3D) - Method in class org.orekit.frames.FieldTransform

Transform a position vector (including translation effects).

transformPosition(Vector3D) - Method in class org.orekit.frames.Transform

Transform a position vector (including translation effects).

TransformProvider - Interface in org.orekit.frames

Interface for Transform providers.

TransformProviderUtils - Class in org.orekit.frames

Utility for Transform providers.

transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform

Transform TimeStampedFieldPVCoordinates including kinematic effects.

transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform

Transform FieldPVCoordinates including kinematic effects.

transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.FieldTransform

Transform TimeStampedPVCoordinates including kinematic effects.

transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform

Transform PVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform

Transform TimeStampedFieldPVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform

Transform TimeStampedFieldPVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.FieldTransform

Transform TimeStampedPVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.Transform

Transform TimeStampedPVCoordinates including kinematic effects.

transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.FieldTransform

Transform a vector (ignoring translation effects).

transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.Transform

Transform a vector (ignoring translation effects).

transformVector(Vector3D) - Method in class org.orekit.frames.FieldTransform

Transform a vector (ignoring translation effects).

transformVector(Vector3D) - Method in class org.orekit.frames.Transform

Transform a vector (ignoring translation effects).

TRANSMIT_BAND - org.orekit.files.ccsds.Keyword

Frequency band for transmitted frequencies.

TRANSMIT_DELAY_1 - org.orekit.files.ccsds.Keyword

Meta-data: Transmit delays list (up to 5).

TRANSMIT_DELAY_2 - org.orekit.files.ccsds.Keyword

Second.

TRANSMIT_DELAY_3 - org.orekit.files.ccsds.Keyword

Second.

TRANSMIT_DELAY_4 - org.orekit.files.ccsds.Keyword

Second.

TRANSMIT_DELAY_5 - org.orekit.files.ccsds.Keyword

Second.

TRANSMIT_FREQ_1 - org.orekit.files.ccsds.Keyword

Data: Transmitted frequencies [Hz].

TRANSMIT_FREQ_2 - org.orekit.files.ccsds.Keyword

Transmitted frequency 2.

TRANSMIT_FREQ_3 - org.orekit.files.ccsds.Keyword

Transmitted frequency 3.

TRANSMIT_FREQ_4 - org.orekit.files.ccsds.Keyword

Transmitted frequency 4.

TRANSMIT_FREQ_5 - org.orekit.files.ccsds.Keyword

Transmitted frequency 5.

TRANSMIT_FREQ_RATE_1 - org.orekit.files.ccsds.Keyword

Data: Transmitted frequencies rates [Hz/s].

TRANSMIT_FREQ_RATE_2 - org.orekit.files.ccsds.Keyword

Transmitted frequency rate 2.

TRANSMIT_FREQ_RATE_3 - org.orekit.files.ccsds.Keyword

Transmitted frequency rate 3.

TRANSMIT_FREQ_RATE_4 - org.orekit.files.ccsds.Keyword

Transmitted frequency rate 4.

TRANSMIT_FREQ_RATE_5 - org.orekit.files.ccsds.Keyword

Transmitted frequency rate 5.

TRIGGER_ONLY_DECREASING_EVENTS - org.orekit.propagation.events.FilterType

Constant for triggering only decreasing events.

TRIGGER_ONLY_INCREASING_EVENTS - org.orekit.propagation.events.FilterType

Constant for triggering only increasing events.

TROPO_DRY - org.orekit.files.ccsds.Keyword

Data: TROPO DRY [m].

TROPO_WET - org.orekit.files.ccsds.Keyword

Data: TROPO WET [m].

TroposphericDSConverter - Class in org.orekit.estimation.measurements.modifiers

Converter for states and parameters arrays.

TroposphericDSConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter

Simple constructor.

TroposphericModel - Interface in org.orekit.models.earth

Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.

TRUE - org.orekit.orbits.PositionAngle

True angle.

TRUE_ANOMALY - org.orekit.files.ccsds.Keyword

Orbit true anomaly.

trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit

Computes the eccentric latitude argument from the true latitude argument.

trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit

Computes the eccentric longitude argument from the true longitude argument.

trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Computes the eccentric latitude argument from the true latitude argument.

trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Computes the eccentric longitude argument from the true longitude argument.

trueToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit

Computes the elliptic eccentric anomaly from the true anomaly.

trueToEllipticEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Computes the elliptic eccentric anomaly from the true anomaly.

trueToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit

Computes the hyperbolic eccentric anomaly from the true anomaly.

trueToHyperbolicEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

Computes the hyperbolic eccentric anomaly from the true anomaly.

tryAdvance(FieldSpacecraftState<T>, FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState

Try to accept the current history up to the given time.

tryAdvance(SpacecraftState, OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState

Try to accept the current history up to the given time.

tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

tsi from SPTRCK #3.

TT - org.orekit.files.ccsds.CcsdsTimeScale

Terrestrial Time.

TTScale - Class in org.orekit.time

Terrestrial Time as defined by IAU(1991) recommendation IV.

TURNAROUND_DENOMINATOR - org.orekit.files.ccsds.Keyword

Meta-data: Turn-around ratio denominator.

TURNAROUND_NUMERATOR - org.orekit.files.ccsds.Keyword

Meta-data: Turn-around ratio numerator.

TurnAroundRange - Class in org.orekit.estimation.measurements

Class modeling a turn-around range measurement using a master ground station and a slave ground station.

TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange

Deprecated.

as of 9.3, replaced by TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite)

TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange

Deprecated.

as of 9.3, replaced by TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite)

TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange

Simple constructor.

TurnAroundRangeBuilder - Class in org.orekit.estimation.measurements.generation

Builder for TurnAroundRange measurements.

TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder

Simple constructor.

TurnAroundRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical TurnAroundRange measurement with ionospheric delay.

TurnAroundRangeIonosphericDelayModifier(IonosphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier

Constructor.

TurnAroundRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical turn-around TurnAroundRange measurement with tropospheric delay.

TurnAroundRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier

Constructor.

U

UNABLE_TO_COMPUTE_DSST_MEAN_PARAMETERS - org.orekit.errors.OrekitMessages

UNABLE_TO_COMPUTE_ECKSTEIN_HECHLER_MEAN_PARAMETERS - org.orekit.errors.OrekitMessages

UNABLE_TO_COMPUTE_HYPERBOLIC_ECCENTRIC_ANOMALY - org.orekit.errors.OrekitMessages

UNABLE_TO_FIND_FILE - org.orekit.errors.OrekitMessages

UNABLE_TO_FIND_RESOURCE - org.orekit.errors.OrekitMessages

UNABLE_TO_GENERATE_NEW_DATA_AFTER - org.orekit.errors.OrekitMessages

UNABLE_TO_GENERATE_NEW_DATA_BEFORE - org.orekit.errors.OrekitMessages

UNABLE_TO_PARSE_LINE_IN_FILE - org.orekit.errors.OrekitMessages

UNABLE_TO_READ_JPL_HEADER - org.orekit.errors.OrekitMessages

UNDEFINED - org.orekit.files.sp3.SP3File.SP3FileType

undefined file format.

UNEXPECTED_DATA_AFTER_LINE_IN_FILE - org.orekit.errors.OrekitMessages

UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages

UNEXPECTED_END_OF_FILE_AFTER_LINE - org.orekit.errors.OrekitMessages

UNEXPECTED_FILE_FORMAT_ERROR_FOR_LOADER - org.orekit.errors.OrekitMessages

UNEXPECTED_TWO_ELEVATION_VALUES_FOR_ONE_AZIMUTH - org.orekit.errors.OrekitMessages

UnivariateProcessNoise - Class in org.orekit.estimation.sequential

Provider for a temporal evolution of the process noise matrix.

UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise

Simple constructor.

UnixCompressFilter - Class in org.orekit.data

Filter for Unix compressed data.

UnixCompressFilter() - Constructor for class org.orekit.data.UnixCompressFilter

UNKNOWN - org.orekit.files.ccsds.TDMParser.TDMFileFormat

UKNOWN file format, default format, throw an Orekit Exception if kept this way.

UNKNOWN - org.orekit.forces.gravity.potential.TideSystem

Constant for unknown tide system.

UNKNOWN_ADDITIONAL_STATE - org.orekit.errors.OrekitMessages

UNKNOWN_MONTH - org.orekit.errors.OrekitMessages

UNKNOWN_RINEX_FREQUENCY - org.orekit.errors.OrekitMessages

UNKNOWN_SATELLITE_ANTENNA_CODE - org.orekit.errors.OrekitMessages

UNKNOWN_SATELLITE_SYSTEM - org.orekit.errors.OrekitMessages

UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide un-normalized spherical harmonics coefficients.

UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

Un-normalized spherical harmonics coefficients evaluated at a specific instant.

UNSUPPORTED_FILE_FORMAT - org.orekit.errors.OrekitMessages

UNSUPPORTED_LOCAL_ORBITAL_FRAME - org.orekit.errors.OrekitMessages

UNSUPPORTED_PARAMETER_NAME - org.orekit.errors.OrekitMessages

UNSUPPORTED_TIME_TRANSFORM - org.orekit.errors.OrekitMessages

unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.OrekitException

Recover a OrekitException, possibly embedded in a MathRuntimeException.

unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.TimeStampedCacheException

Recover a TimeStampedCacheException, possibly embedded in a MathRuntimeException.

unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException

Recover a TimeStampedCacheException, possibly embedded in a OrekitException.

UpdatableFrame - Class in org.orekit.frames

Frame whose transform from its parent can be updated.

UpdatableFrame(Frame, Transform, String) - Constructor for class org.orekit.frames.UpdatableFrame

Build a non-inertial frame from its transform with respect to its parent.

UpdatableFrame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.UpdatableFrame

Build a frame from its transform with respect to its parent.

updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Update state by adding all additional states.

updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator

Update state by adding all additional states.

updateMass(double) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Update a spacecraft mass due to maneuver.

updateShortPeriodTerms(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Update the short period terms.

updateShortPeriodTerms(SpacecraftState...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Update the short period terms.

updateShortPeriodTerms(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Update the short period terms.

updateShortPeriodTerms(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Update the short period terms.

updateShortPeriodTerms(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Update the short period terms.

updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.UpdatableFrame

Update the transform from parent frame implicitly according to two other frames.

UpperBounds - Class in org.orekit.propagation.semianalytical.dsst.utilities

Utility class to compute upper bounds for truncation algorithms.

URANUS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for Uranus.

URANUS - org.orekit.files.ccsds.CenterName

Uranus body.

URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Uranus.

USE_P - org.orekit.utils.CartesianDerivativesFilter

Use only positions, ignoring velocities.

USE_PV - org.orekit.utils.CartesianDerivativesFilter

Use positions and velocities.

USE_PVA - org.orekit.utils.CartesianDerivativesFilter

Use positions, velocities and accelerations.

USE_R - org.orekit.utils.AngularDerivativesFilter

Use only rotations, ignoring rotation rates.

USE_RR - org.orekit.utils.AngularDerivativesFilter

Use rotations and rotation rates.

USE_RRA - org.orekit.utils.AngularDerivativesFilter

Use rotations, rotation rates and acceleration.

USEABLE_START_TIME - org.orekit.files.ccsds.Keyword

Start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

USEABLE_STOP_TIME - org.orekit.files.ccsds.Keyword

End of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

USER_DEFINED_X - org.orekit.files.ccsds.Keyword

User defined parameter, where X is replaced by a variable length user specified character string.

usesInterpolation() - Method in class org.orekit.frames.EOPHistory

Check if the instance uses interpolation on tidal corrections.

UT1 - org.orekit.files.ccsds.CcsdsTimeScale

Universal Time.

UT1Scale - Class in org.orekit.time

Universal Time 1.

UT1Scale(EOPHistory, UTCScale) - Constructor for class org.orekit.time.UT1Scale

Simple constructor.

UTC - org.orekit.files.ccsds.CcsdsTimeScale

Universal Coordinated Time.

UTC - org.orekit.files.sp3.SP3File.TimeSystem

Coordinated Universal Time.

UTCScale - Class in org.orekit.time

Coordinated Universal Time.

UTCTAIBulletinAFilesLoader - Class in org.orekit.time

Loader for UTC-TAI extracted from bulletin A files.

UTCTAIBulletinAFilesLoader(String) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader

Build a loader for IERS bulletins A files.

UTCTAIHistoryFilesLoader - Class in org.orekit.time

Loader for UTC versus TAI history files.

UTCTAIHistoryFilesLoader() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader

Build a loader for UTC-TAI history file.

UTCTAIOffsetsLoader - Interface in org.orekit.time

Interface for loading UTC-TAI offsets data files.

UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control

V

validFrom() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the start of the validity period for this model.

validityEnd() - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider

Get end of validity for this provider.

validityEnd() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider

Get end of validity for this provider.

validityStart() - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider

Get start of validity for this provider.

validityStart() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider

Get start of validity for this provider.

validTo() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the end of the validity period for this model.

value(double) - Method in class org.orekit.data.PolynomialNutation

Evaluate the value of the polynomial.

value(double, double) - Method in interface org.orekit.gnss.antenna.PhaseCenterVariationFunction

Evaluate phase center variation in one signal direction.

value(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate a set of Poisson series.

value(BodiesElements) - Method in class org.orekit.data.PoissonSeries

Evaluate the value of the series.

value(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate a set of Poisson series.

value(FieldBodiesElements<T>) - Method in class org.orekit.data.PoissonSeries

Evaluate the value of the series.

value(Orbit) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms

Evaluate the contributions of the short period terms.

value(SpacecraftState) - Method in interface org.orekit.utils.StateFunction

Evaluate the function.

value(SpacecraftState) - Method in interface org.orekit.utils.StateJacobian

Evaluate the Jacobian of the function.

value(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Compute the value of the coefficient.

value(AbsoluteDate) - Method in interface org.orekit.time.TimeScalarFunction

Compute a function of time.

value(AbsoluteDate) - Method in interface org.orekit.time.TimeVectorFunction

Compute a function of time.

value(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the value of the gravity field.

value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScalarFunction

Compute a function of time.

value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeVectorFunction

Compute a function of time.

value(ParameterDriver) - Method in interface org.orekit.utils.ParameterFunction

Evaluate the function.

value(T) - Method in class org.orekit.data.PolynomialNutation

Evaluate the value of the polynomial.

VALUE_NOT_FOUND - org.orekit.errors.OrekitMessages

valueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter value has been changed.

valueOf(String) - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.data.PolynomialParser.Unit

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.errors.OrekitMessages

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurement.Status

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.CCSDSFrame

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.CcsdsTimeScale

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.CenterName

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.Keyword

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.OEMWriter.InterpolationMethod

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.TDMParser.TDMFileFormat

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3FileType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.TimeSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.TideSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.ITRFVersion

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.LOFType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.Predefined

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.Frequency

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.MeasurementType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.ObservationType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.SatelliteSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.models.earth.ViennaModelType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.orbits.OrbitType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.orbits.PositionAngle

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.events.FilterType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.events.handlers.EventHandler.Action

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.events.handlers.FieldEventHandler.Action

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.time.Month

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.AngularDerivativesFilter

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.CartesianDerivativesFilter

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.IERSConventions

Returns the enum constant of this type with the specified name.

values() - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.data.PolynomialParser.Unit

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.errors.OrekitMessages

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurement.Status

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.CCSDSFrame

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.CcsdsTimeScale

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.CenterName

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.Keyword

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.OEMWriter.InterpolationMethod

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.TDMParser.TDMFileFormat

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sp3.SP3File.SP3FileType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sp3.SP3File.TimeSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.gravity.potential.TideSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.HelmertTransformation.Predefined

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.ITRFVersion

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.LOFType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.Predefined

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.antenna.SatelliteAntennaCode

Deprecated.

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.antenna.SatelliteType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.Frequency

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.MeasurementType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.ObservationType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.SatelliteSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.models.earth.ViennaModelType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.orbits.OrbitType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.orbits.PositionAngle

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.events.FilterType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.events.handlers.EventHandler.Action

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.events.handlers.FieldEventHandler.Action

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.time.Month

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.AngularDerivativesFilter

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.CartesianDerivativesFilter

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.IERSConventions

Returns an array containing the constants of this enum type, in the order they are declared.

VEIS_1950 - org.orekit.frames.Predefined

Veis 1950.

VENUS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Constant for Venus.

VENUS - org.orekit.files.ccsds.CenterName

Venus body.

VENUS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Venus.

VersionedITRF - Class in org.orekit.frames

Specific version of International Terrestrial Reference Frame.

VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_AVAILABLE_FOR_DATE - org.orekit.errors.OrekitMessages

VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_LOADED - org.orekit.errors.OrekitMessages

VIENNA_ONE - org.orekit.models.earth.ViennaModelType

Vienna one tropospheric model.

VIENNA_THREE - org.orekit.models.earth.ViennaModelType

Vienna three tropospheric model.

ViennaModelCoefficientsLoader - Class in org.orekit.models.earth

Loads Vienna tropospheric coefficients a given input stream.

ViennaModelCoefficientsLoader(double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.ViennaModelCoefficientsLoader

Constructor with default supported names.

ViennaModelCoefficientsLoader(String, double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.ViennaModelCoefficientsLoader

Constructor with supported names given by user.

ViennaModelType - Enum in org.orekit.models.earth

Enumerate for Vienna tropospheric model 1 and 3.

ViennaOneModel - Class in org.orekit.models.earth

The Vienna1 tropospheric delay model for radio techniques.

ViennaOneModel(double[], double[], double) - Constructor for class org.orekit.models.earth.ViennaOneModel

Build a new instance.

ViennaThreeModel - Class in org.orekit.models.earth

The Vienna3 tropospheric delay model for radio techniques.

ViennaThreeModel(double[], double[], double, double) - Constructor for class org.orekit.models.earth.ViennaThreeModel

Build a new instance.

VLBI_DELAY - org.orekit.files.ccsds.Keyword

Data: VLBI delay [s].

VNC - org.orekit.frames.LOFType

Constant for Velocity - Normal - Co-normal frame (X axis aligned with velocity, Y axis aligned with orbital momentum).

VVLH - org.orekit.frames.LOFType

Constant for Vehicle Velocity, Local Horizontal frame (Z axis aligned with opposite of position, Y axis aligned with opposite of orbital momentum).

W

w - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Equinoctial frame w vector.

WEAK - org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel

Weak level of activity.

WeatherModel - Interface in org.orekit.models.earth

Defines a surface meteorology model that can be used to compute the different weather parameters (pressure, temperature, ...).

weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model

weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.GlobalPressureTemperatureModel

weatherParameters(double, AbsoluteDate) - Method in interface org.orekit.models.earth.WeatherModel

Calculates the weather parameters of the model.

WGS84_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from WGS84 model: 7.292115e-5 rad/s.

WGS84_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from WGS84 model: .

WGS84_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from WGS84 model: 6378137.0 m.

WGS84_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from WGS84 model: 1.0 / 298.257223563.

WGS84_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from WGS84 model: 3.986004418e14 m³/s².

withConstantElevation(double) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the minimum elevation for detection.

withConstantElevation(double) - Method in class org.orekit.propagation.events.FieldElevationDetector

Setup the minimum elevation for detection.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.ODMParser

Set IERS conventions.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OEMParser

Set IERS conventions.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OMMParser

Set IERS conventions.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OPMParser

Set IERS conventions.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.TDMParser

Set IERS conventions.

withDoodson(int, int) - Method in class org.orekit.data.PoissonSeriesParser

Set up columns for Doodson multipliers and Doodson number.

withElevationMask(ElevationMask) - Method in class org.orekit.gnss.DOPComputer

Set the elevation mask.

withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the elevation mask for detection using the passed in mask object.

withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.FieldElevationDetector

Setup the elevation mask for detection using the passed in mask object.

withFileFormat(TDMParser.TDMFileFormat) - Method in class org.orekit.files.ccsds.TDMParser

Set file format.

withFirstDelaunay(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up first column of Delaunay multiplier.

withFirstPlanetary(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up first column of planetary multiplier.

withFunction(ToDoubleFunction<SpacecraftState>) - Method in class org.orekit.propagation.events.FunctionalDetector

Create a new event detector with a new g function, keeping all other attributes the same.

withGamma(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up column of GMST tide multiplier.

withGFunction(FunctionalDetector.GFunction) - Method in class org.orekit.propagation.events.FunctionalDetector

Deprecated.

Use FunctionalDetector.withFunction(ToDoubleFunction) instead. Will be removed in next major release.

withHandler(EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the event handler to call at event occurrences.

withHandler(FieldEventHandler<? super D, T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the event handler to call at event occurrences.

withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.ODMParser

Set international designator.

withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OEMParser

Set international designator.

withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OMMParser

Set international designator.

withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OPMParser

Set international designator.

withMargin(double) - Method in class org.orekit.propagation.events.GeographicZoneDetector

Setup the detector margin.

withMaxCheck(double) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the maximum checking interval.

withMaxCheck(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the maximum checking interval.

withMaxIter(int) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the maximum number of iterations in the event time search.

withMaxIter(int) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the maximum number of iterations in the event time search.

withMinElevation(double) - Method in class org.orekit.gnss.DOPComputer

Set the minimum elevation.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ODMParser

Set initial date.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OEMParser

Set initial date.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OMMParser

Set initial date.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OPMParser

Set initial date.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMParser

Set initial date.

withMu(double) - Method in class org.orekit.files.ccsds.ODMParser

Set gravitational coefficient.

withMu(double) - Method in class org.orekit.files.ccsds.OEMParser

Set gravitational coefficient.

withMu(double) - Method in class org.orekit.files.ccsds.OMMParser

Set gravitational coefficient.

withMu(double) - Method in class org.orekit.files.ccsds.OPMParser

Set gravitational coefficient.

withOptionalColumn(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up optional column.

withPenumbra() - Method in class org.orekit.propagation.events.EclipseDetector

Setup the detector to penumbra detection.

withPenumbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Setup the detector to penumbra detection.

withPolynomialPart(char, PolynomialParser.Unit) - Method in class org.orekit.data.PoissonSeriesParser

Set up polynomial part parsing.

withReferenceFrame(Frame) - Method in class org.orekit.attitudes.Attitude

Get a similar attitude with a specific reference frame.

withReferenceFrame(Frame) - Method in class org.orekit.attitudes.FieldAttitude

Get a similar attitude with a specific reference frame.

withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the elevation detector to use an atmospheric refraction model in its calculations.

withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.FieldElevationDetector

Setup the elevation detector to use an atmospheric refraction model in its calculations.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.ODMParser

Set EOP interpolation method.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OEMParser

Set EOP interpolation method.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OMMParser

Set EOP interpolation method.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OPMParser

Set EOP interpolation method.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.TDMParser

Set EOP interpolation method.

withSinCos(int, int, double, int, double) - Method in class org.orekit.data.PoissonSeriesParser

Set up columns of the sine and cosine coefficients.

withSwitch(int, int) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00

Change a switch.

withThreshold(double) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the convergence threshold.

withThreshold(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the convergence threshold.

withUmbra() - Method in class org.orekit.propagation.events.EclipseDetector

Setup the detector to full umbra detection.

withUmbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Setup the detector to full umbra detection.

WMM - org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel

World Magnetic Model.

write(Appendable, EphemerisFile) - Method in class org.orekit.files.ccsds.OEMWriter

Write the passed in EphemerisFile using the passed in Appendable.

write(Appendable, EphemerisFile) - Method in interface org.orekit.files.general.EphemerisFileWriter

Write the passed in EphemerisFile using the passed in Appendable.

write(String, EphemerisFile) - Method in interface org.orekit.files.general.EphemerisFileWriter

Write the passed in EphemerisFile to a file at the output path specified.

writeEphemerisLine(TimeStampedPVCoordinates) - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment

Write a single ephemeris line according to section 5.2.4.

writeHeader() - Method in class org.orekit.files.ccsds.StreamingOemWriter

Writes the standard OEM header for the file.

writeMetadata() - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment

Write the ephemeris segment metadata.

WRONG_COLUMNS_NUMBER - org.orekit.errors.OrekitMessages

X

X - org.orekit.files.ccsds.Keyword

Position vector X-component.

X_DOT - org.orekit.files.ccsds.Keyword

Velocity vector X-component.

xl - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

L from SPTRCK #3.

xmdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for mean anomaly (M) computation.

XML - org.orekit.files.ccsds.TDMParser.TDMFileFormat

XML format.

xn0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original recovered mean motion.

xnodcf - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for raan (OMEGA) computation.

xnode - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final RAAN.

xnodot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for raan (OMEGA) computation.

Y

Y - org.orekit.files.ccsds.Keyword

Position vector Y-component.

Y_DOT - org.orekit.files.ccsds.Keyword

Velocity vector Y-component.

YawCompensation - Class in org.orekit.attitudes

This class handles yaw compensation attitude provider.

YawCompensation(Frame, GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation

Creates a new instance.

YawSteering - Class in org.orekit.attitudes

This class handles yaw steering law.

YawSteering(Frame, GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering

Creates a new instance.

YUMAParser - Class in org.orekit.gnss

This class reads Yuma almanac files and provides GPS almanacs.

YUMAParser(String) - Constructor for class org.orekit.gnss.YUMAParser

Simple constructor.

Z

Z - org.orekit.files.ccsds.Keyword

Position vector Z-component.

Z_DOT - org.orekit.files.ccsds.Keyword

Velocity vector Z-component.

ZERO - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

0 represented as a polynomial.

ZERO - Static variable in class org.orekit.utils.PVCoordinates

Fixed position/velocity at origin (both p, v and a are zero vectors).

ZERO_TIDE - org.orekit.forces.gravity.potential.TideSystem

Constant for zero-tide gravity fields.

ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider

Pattern for name of zip/jar archives.

ZipJarCrawler - Class in org.orekit.data

Helper class for loading data files from a zip/jar archive.

ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file on filesystem.

ZipJarCrawler(ClassLoader, String) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file in classpath.

ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file in classpath.

ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file on network.

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